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  • [Project Topics] Hayabusa2 additional ion engine operation for Earth swing-by

    Topics List

    Sep. 2, 2015 Updated
    Hayabusa2 additional ion engine operation for Earth swing-by

    On Sept. 1 (Tue.) and 2 (Wed.), the ion engine of the Hayabusa2 was additionally operated in order to increase the orbit control accuracy for the Earth swing-by.
    The additional jet emission was completed as scheduled, and the ion engine was operated for about 12 hours in total.
    We will analyze telemetry data (data sent from the explorer to indicate its condition) in detail to confirm the status of the engine during the operation and orbit control before and after the emission.
    Figure: Positional relation of Hayabusa2, the Earth, the Sun, and Asteroid 1999JU3 (Schematic as of Sept. 1, 2015)

    Hayabusa2 additional ion engine operation for Earth swing-by

    Jul. 22, 2015 Updated
    Naming Proposal Campaign: Become a godparent of asteroid “1999 JU3”, destination of Hayabusa2!

    JAXA is holding a naming proposal campaign to christen the asteroid “1999 JU3″,which the Hayabusa2 is scheduled to visit in June or July 2018. Why don’t you try to become a godparent of the asteroid?
    The application period is from 1:30 p.m. on July 22 thru 11:59 p.m. on August 31 (Japan Standard Time.)

    August 31, 2015 at 11:59 p.m. (Japan Standard Time). (Extended from 10:00)

    Jun. 8, 2015 Updated
    Hayabusa2 second ion engine continuous operation completed

    The Hayabusa2 has been continuously operating its ion engine for the second time since June 2, and successfully completed its operations at 0:25 a.m. on June 7 (Japan Standard Time.) The second continuous operation lasted for 102 hours as scheduled.
    The Hayabusa2 performed the ion engine continuous operation in preparation for the Earth swing-by planned in December, and the total hours of the first and second operations (409 hours and 102 hours respectively) reached 511 hours.
    The ion engine operation may be conducted again if needs arise for subtle orbit change after carefully examining the second operation result.

    Hayabusa2 second ion engine continuous operation completed

    Apr. 10, 2015 Updated
    Baton pass to new Hayabusa2 project manager

    The Hayabusa2 is stably flying in space. The new fiscal year has just started in Japan, and JAXA is taking a new step as we became a National Research and Development Agency from the previous independent administrative agency. The Hayabusa2 project is also taking a fresh step with a new team, including handing the baton over to a new project manager. All members of the project are engaged in the mission with a fresh mindset.

    Message from New Project Manager Yuichi Tsuda

    The Hayabusa2 is stably flying since its launch and smoothly continuing it interplanetary cruising. I can, therefore, take over the mission at the best condition from my predecessor, former Project Manager Hitoshi Kuninaka, who led the development of the project. With many operation experts joining the new team, we would like to successfully send the Hayabusa2 to the asteroid 1999JU3, and have it come home safely.
    The Hayabusa2 mission is challenging an unexplored field. We would like to contribute to enhancing the value of technology, science and space exploration through our accomplishments in traveling through the solar system in this six-year mission.

    Message from Former Project Manager Hitoshi Kuninaka

    As the development phase is over, Hayabusa2’s deep space exploration has started.
    At the beginning of this fiscal year, a multiple number of our project members including myself were subject to personnel changes. Our team worked well with good team spirit to tackle and overcome various obstacles and difficulties. Therefore, I felt a bit disappointed to see part of the team was shuffled. Having said that, those who remain in the team as well as the leaving members vow to work hard and do our best using our expertise in space projects no matter what department we are assigned to. Your continued support for the Hayabusa2 is very much appreciated.

    Photo: left: New Project Manager Yuichi Tsuda, right: Former Project Manager Hitoshi Kuninaka

    Baton pass to new Hayabusa2 project manager

    Mar. 5, 2015 Updated
    Hayabusa2 initial functional confirmation completed and moved to cruising phase to asteroid

    The Asteroid Explorer “Hayabusa2,” launched on Dec. 3, 2014, completed its initial functional confirmation period of about three months. The explorer was moving to the cruising phase on March 3 while heading to the asteroid “1999 JU3.”
    The Hayabusa2 is in good health. It will be under preparatory operation including speed increase by continuous operation of the ion engines for an Earth swing-by scheduled in Nov. or Dec., 2015.

    Hayabusa2 initial functional confirmation completed and moved to cruising phase to asteroid

    Feb. 3, 2015 Updated
    Hayabusa2 in great shape – Initial functional confirmation going smoothly

    The Hayabusa2, launched on Dec. 3, 2014 (JST), is now undergoing the initial functional confirmation. Basic operations and performance of onboard instruments and ground systems have been tested one by one as of the end of January.
    Here are some major examples of what we confirmed.

    1. Ion engine test operation (one unit at a time)
      Four ion engines were being operated one by one. A thrust of 7-10 mN was generated on the orbit for the first time.
    2. Establishing communication by Ka band communication equipment (Between Jan. 5 to 10, 2015)
      Communication was successful between the Hayabusa2 and NASA DSN stations to establish deep-space Ka-band communication for the first time for a Japanese space explorer. Ka-band communication will be used to send observation data during the mission for the Hayabusa2 to stay near the asteroid.
    3. Ion engine can autonomously operate for 24 hours.
      Long duration of autonomous operation (*1) with two or three ion engines was tested, and 24-hour continuous operation was attained.
      The maximum thrust was confirmed to be about 28 mN, which is the expected value.

    The explorer is currently in good shape.
    We will further confirm the coordinated function of multiple instruments of the Hayabusa2, and plan to move to the cruise operation phase (*2) sometime in March.

    *1 The autonomous operation is automatic control of an engine without instructions from the ground.
    *2 The mode of full-scale navigation operation toward the asteroid through acceleration and orbit control by ion engine thrust.

    Hayabusa2 in great shape – Initial functional confirmation going smoothly

    Dec. 5, 2014 Updated
    Hayabusa2 flying smoothly!

    JAXA confirmed the completion of a sequence of the important operations for the “Hayabusa2” mission. With this confirmation, the critical operation phase* of the Hayabusa2 was completed.
    The explorer is now in a stable condition.

    We would like to express our sincere appreciation to all parties and personnel concerned for their support and cooperation with the Hayabusa2 launch and tracking control operations.
    In addition, we would also like to ask for your continued cooperation and support for the long-term Hayabusa2 space exploration mission.

    Please send your support messages for the mission! (you can send a message from Hayabusa2 Project page or tweet with hashtag #hayabusa2).

    Hayabusa2 flying smoothly!

    Dec. 3, 2014 Updated
    “Hayabusa2” successfully launched!

    H-IIA F26 with the Asteroid Explorer “Hayabusa2” onboard launched at 1:22:04 p.m. on Dec 3, 2014 (JST) from the Tanegashima Space Center.
    The rocket flew smoothly, and, at about approximately one hour, 47 minutes and 21 seconds after liftoff, “Hayabusa2” was separated from the H-IIA F26. We will update you with the latest information on the “Hayabusa2” on the project page.
    Please send your support messages for the mission! (you can send a message from Hayabusa2 Project page or tweet with hashtag #hayabusa2).

    Nov. 30, 2014 Updated
    “Hayabusa2” Launch rescheduled to 1:22:04 p.m. on December 3 (Mon.) 2014

    Mitsubishi Heavy Industries, Ltd. and JAXA have decided to postpone the launch of “Hayabusa2” and piggyback payloads by the H-IIA F26 to 1:22:04 p.m. on Dec 3 (Wed. JST).

    The live launch report will begin at 12:25 p.m. on December 3 (Mon. , JST). The report will be broadcast through the Internet.
    Please send your support messages for the mission! (you can send a message from Hayabusa2 Project page or tweet with hashtag #hayabusa2).

    We decided to postpone as a result of the go/no go decision meeting today which carefully checked the weather forecast and found that strong wind exceeding the weather restrictions was projected around the launch pad at the scheduled launch time on the previous schedule launch day of Dec. 1 (Mon.), 2014.
    *The launch may be delayed further depending on weather conditions and other factors.

    Nov. 29, 2014 Updated
    “Hayabusa2” Launch rescheduled to 1:22:43 p.m. on December 1 (Mon.) 2014

    The launch of the Asteroid Explorer “Hayabusa2” and three micro piggyback payloads by the H-IIA Launch Vehicle No. 26 was rescheduled at 1:22:43 p.m. on December 1 (Mon. Japan Standard Time, JST) after carefully studying the weather conditions.
    Accordingly, the live launch report will begin at 12:25 p.m. on December 1 (Mon. , JST). The report will be broadcast through the Internet.
    Please send your support messages for the mission, or tweet it including the hashtag #hayabusa2.

    Nov. 28, 2014 Updated
    Hayabusa2 launch postponement

    H-IIA Launch Vehicle No.26 with the Asteroid Explorer “Hayabusa2” onboard has been rescheduled as clouds including a freezing layer that exceeds the restrictions for suitable weather are forecast to be generated at around the scheduled launch time on November 30 (Sun.), 2014 (Japan Standard Time.)
    The new launch day will be announced as soon as it is determined.

    Hayabusa2 launch postponement

    Nov. 27, 2014 Updated
    New movie “Ready to Face New Challenges -Hayabusa2- “

    The new video clip titled “Ready to Face New Challenges -Hayabusa2- ” was uploaded to the YouTube.
    It has been four years since the Hayabusa’s dramatic return from space,bringing back the world’s first samples from an asteroid. To further clarify the mystery of the origin and evolution of human beings, the Hayabusa2 is leaving for space. This video explains the special features and significance of the Hayabusa2 mission in an easy and simple manner.

    Nov. 4, 2014 Updated
    “Hayabusa2″ Launch Live Broadcast (by H-IIA F26)

    JAXA will broadcast a live report of the Asteroid Explorer Hayabusa2’s launch by the H-IIA Launch Vehicle No.26 (H-IIA F26) from the Tanegashima Space Center. The report will cover launch events from the liftoff to the payload separation from the launch vehicle.

    Program summary

    The broadcast program consists of two parts. The first half mainly focuses on launch events prior to and after liftoff. Then the latter half covers events before and after the Hayabusa2’s separation from the launch vehicle.

    *Please be aware that the time schedule of the program is subject to change due to progress of the launch operations.

    Program contents

    Part I
    Prior and after liftoff of H-IIA F26/Hayabusa2

    • Introduction of the Hayabusa2 mission including a VTR of its preparation operation
    • Introduction of piggyback payloads
    • Live launch report from the control room

    *The scheduled launch time is 1:24 p.m.

    Part I broadcast day and time
    12:30 p.m. thru 1:45 p.m. (75 minutes) on Nov. 30 (Sun.)

    • Prior to and after the Hayabusa2’s separation from the launch vehicle

    * Images of piggyback payloads’ separation will NOT be broadcast.
    * Hayabusa2’s separation is scheduled to take place one hour and 47 minutes after liftoff.

    Part II broadcast day and time
    3:00 p.m. to 3:30 p.m. (30 minutes) on Nov. 30 (Sun.)

    Internet live broadcast

    JAXA will distribute our live report through the following Internet channels.

    * The copyright of the live broadcast belongs to JAXA.
    * Please be aware that a slight time lag up to a few minutes may occur due to the Internet’s characteristics.

    We are welcoming support messages at the special site. Please send your messages for the mission, or tweet it. To tweet on Twitter, please attach the hashtag, #hayabusa2.
    Click the following link to send a message to JAXA.

    “Hayabusa2

    Sep. 30, 2014 Updated
    New voyager to travel deep into space! Hayabusa2 to be launched on Nov. 30

    The launch date and time for the H-IIA Launch Vehicle No. 26 (H-IIA F26) with the Asteroid Explorer “Hayabusa2” onboard was decided to be at 1:24:48 p.m. on November 30 (Sunday), 2014 (Japan Standard Time)*.
    Launch site is Yoshinobu Launch Complex at the Tanegashima Space Center.
    * Launch time will be set for each launch day if the launch is delayed.

    The latest information about “Hayabusa2” and its launch preparation status will be updated on the “Hayabusa2” project page.
    We welcome your support message for the Hayabusa2.
    Please send your support messages for the mission, or tweet it including the hashtag #hayabusa2.

    New voyager to travel deep into space! Hayabusa2 to be launched on Nov. 30

    Sep. 5, 2014 Updated
    Hayabusa2 revealed to the media

    The Asteroid Explorer “Hayabusa2” was shown to the media at Sagamihara Campus on August 31, 2014.

    The Hayabusa2 is the successor of the Hayabusa, which captured sample particles from an asteroid and returned to the Earth in 2010. By capitalizing on the experience of the Hayabusa, the Hayabusa2 aims at acquiring samples and bringing them back from the C-type asteroid “1999JU3” to elucidate the origin and evolution of the solar system and material for life.

    “I am bracing for the new voyage of the Hayabusa2.” said Project Manager Kuninaka.
    The Hayabusa2 will be transferred to the Tanegashima Space Center for its launch in this winter after its final check there.

    Hayabusa2 revealed to the media

    Nov. 20, 2013 Updated
    Hayabusa2 Small Carry-on Impactor undergoes test

    Hayabusa2’s Small Carry-on Impactor (SCI) underwent a test in October, 2013.
    The SCI is a device to create an artificial crater of the asteroid 1999JU3, which the Hayabusa 2 will travel toward. By making and observing an artificial crater, we can acquire data not only about the surface but also about the inside of the asteroid. In addition, by sampling near the crater, we can collect inside samples of the asteroid.
    Hayabusa2 applies a method to throw a metal projectile against the asteroid with high speed to create an artificial crater. Through the test this time, we confirmed the accelerating part of the projectile while aiming to verify if its speed, configuration, and thrown direction precision met the design when the pyrotechnics, which were comparable to those of actual ones for the flight, were ignited to set off the projectile.
    The test results were very impressive as the speed and configuration were almost as designed, and the direction precision was also good as the SCI precisely hit a target that was 100 meters away. We were able to successfully complete the performance confirmation test of the SCI pyrotechnic part.

    Hayabusa2 SCI test [JAXA Digital Archives]

    Hayabusa2 Small Carry-on Impactor undergoes test

    Jul. 17, 2013 Updated
    Campaign extended till August 9 (Fri.)!
    – Let’s attach your name and message to Hayabusa2 –

    JAXA has been conducting a campaign to attach names and messages of Hayabusa2 mission supporters from all over the world to the space probe! We would love to share this superb moment and feeling of achievement with you through this campaign.

    We would like to express our sincere appreciation to all of you who joined the campaign since it began on April 10 till today. Also we appreciate your cooperation for registering or sending your names and messages on time. Thank you very much.

    As we read the support messages for the Hayabusa2, we strongly felt that we would like to support this mission by being united with more of you.
    Luckily, the Hayabusa2 manufacturing schedule has allowed us to extend the campaign period!

    We are looking forward to hearing from more of you as an individual and/or as a community such as a family, a school or a company, and/or with your friends!

    With the Hayabusa2
    Let’s go to asteroid 1999 JU3, and return to Earth

    Jun. 14, 2013 Updated
    Hayabusa2 completes first integration test

    All processes of the Hayabusa2’s first integration test since January this year were completed on June 7. The test aimed at installing all onboard devices onto the satellite structure and confirming interfaces among them. During the mass property measurement, the last process of the integration test, the “Hayabusa2” exposed its full shape for the first time with all devices for the test installed.
    We will remove each device from the main body of the Hayabusa2, then the devices will be given their final touches. They will be tested again and assembled again to the explorer for the next-phase test. All the project team members will do our best as we have done to steadily implement the Hayabusa2 project.

    Mar. 29, 2013 Updated
    Hayabusa2 can carry your names and messages to space

    JAXA is holding a campaign to record your names, messages and illustrations onboard the asteroid probe Hayabusa2.
    Hayabusa2 is scheduled to be launched by the H-IIA launch vehicle in FY2014, then arrive at an asteroid in 2018 and investigate it for about one and half years, before returning to the earth in 2020.
    The campaign will start from April 10. We welcome your participation!

    Dec. 27, 2012 Updated
    Hayabusa2 revealed before the first integration test

    On Dec. 26, the Hayabusa2 was revealed at the Sagamihara Campus. As its design was completed this spring, the Hayabusa2 will soon undergo the first integration test to confirm the interfaces among onboard devices as well as between the devices and the explorer’s bus after assembling them onto the bus. Also, the flight models of the Hayabusa2’s main body and solar array paddles have already been manufactured, thus those models will be verified through a vibration test. In addition, the exposed environment for the onboard devices will also be measured. JAXA is developing the Hayabusa2 to be ready for its launch in FY2014.

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  • [Earth Observation Research Center (EORC)] Seen from Space – Release of JAXA Himawari Monitor

    Earth Observation Research Center (EORC) of Japan Aerospace Exploration Agency (JAXA) has released a new webpage “JAXA Himawari Monitor” showing the color images and the quicklook images of the geophysical data from the geostationary satellite of Japan Meteorological Agency (JMA), Himawari-8.

    JAXA and JMA has exchanged the agreement on the distribution and the release of meteorological data and under this agreement, EORC has released the data from Himawari-8 to research communities and has been creating the geophysical data that are consistent with the JAXA’s earth observation satellites in order to release them widely to general public. Other than releasing the images in JAXA Himawari Monitor, EORC also stated to distribute via FTP the Himawari Standard Data and the geophysical data produced by JAXA.

    The Himawari Standard Data includes the visible to infrared radiances (Band 1 to 16) for three regions of Full Disk (global), Japan Area and Target Area. The observation data can be achieved every 10 minutes for Full Disk and every 2.5 minutes for Japan Area and Target Area. Using the observation bands that enable the world’s first “color image” from geostationary satellite, one of the advanced aspects of Himawari-8, JAXA Himawari Monitor shows the visible RGB composite images (Figure 1).

    An example of visible RGB image in JAXA Himawari Monitor
    Figure 1. An example of visible RGB image in JAXA Himawari Monitor

    In addition, for the Himawari geophysical data, JAXA produces the properties of atmospheric particles (called aerosols) such as desert dusts and PM2.5 and the sea surface temperature. Both applied the algorithm developed for the JAXA’s earth observation satellites, including the Global Change Observation Mission – Climate (GCOM-C) satellite, in order to produce, in the future, the dataset that are consistent between the satellites and can compensate each other’s observations.
    The aerosol property product (Figure 2) is being produced every 10 minutes in the daytime with the spatial resolution of 5km. Current product is a beta version and will increase the quality through the ground validation.

    An example the atmospheric particle property (aerosol optical depth) in JAXA Himawari Monitor
    Figure 2. An example the atmospheric particle property (aerosol optical depth) in JAXA Himawari Monitor

    There are two kinds of sea surface temperature products: an ordinary product and a nighttime product. The ordinary sea surface temperature product (Figure 3) is a dataset produced every 10 minutes, regardless of day or night, with the spatial resolution of 2km. In order to reduce the missing area by clouds, hourly averaged products are also created. The nighttime sea surface temperature uses Band 7 (3.9 µm wavelength) and, although it can only be retrieved at nighttime, its advantage is in its high accuracy. The dataset of nighttime sea surface temperature is hourly averaged product with the spatial resolution of 2km.

    An example of sea surface temperature in JAXA Himawari Monitor
    Figure 3. An example of sea surface temperature in JAXA Himawari Monitor

    Explanation of the Images:

    Satellite: Himawari-8(JMA)
    Sensor: Advanced Himawari Imager:AHI(JMA)
    Date: 06:00UTC on Aug. 31, 2015(Fig.1 , Fig.3)
    03:30UTC on Sep. 1, 2015(fig.2)

    Related Sites:

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  • [Project Topics] KOUNOTORI5 captured and berthed at the ISS

    Topics List

    Aug. 25, 2015 Updated
    KOUNOTORI5 captured and berthed at the ISS

    The “KOUNOTORI5” launched by the H-IIB F5 on Aug. 19 (Wed. Japan Standard Time) was captured by the robotic arm of the International Space Station (ISS), which was maneuvered by Astronaut Kimiya Yui, at 7:29 p.m. on August 24 (Mon. JST). The HTV5 was then successfully berthed at the ISS at 2:28 a.m. on August 25 (Tue. JST).
    The internal cargo as well as external cargo, such as CALET, on the KOUNOTORI5 will be unloaded by the onboard crew. (Photo: NASA TV)

    KOUNOTORI5 captured and berthed at the ISS

    Aug. 19, 2015 Updated
    KOUNOTORI5 successfully launched by H-IIB F5!

    The KOUNOTORI5, a regular cargo transporter to space, was launched by the H-IIB Launch Vehicle No.5 (H-IIB F5) at 8:50:49 p.m. on August 19 (Wed.) 2015 (Japan Standard Time, JST) from the Tanegashima Space Center. The launch vehicle flew smoothly, and, at about 14 minutes and 54 seconds after liftoff, the separation of the KOUNOTORI5 was confirmed.
    The KOUNOTORI5 will fly near the International Space Station, and Astronaut Yui will maneuver the robotic arm to capture it. We plan to broadcast his performance through the Internet from around 7:05 p.m. on Aug. 24 (Mon.) Please don’t miss it!

    KOUNOTORI5 successfully launched by H-IIB F5!

    Aug. 17, 2015 Updated
    KOUNOTORI5 launch rescheduled to 8:50:49 p.m. on August 19 (Wed.) 2015

    The KOUNOTORI5(HTV5)/H-IIB F5 launch was postponed to 8:50:49 p.m. on August 19 due to adverse weather.
    Accordingly, the live launch report will begin at 8:00 p.m. on August 19 (Wed. , JST). The report will be broadcast through the Internet.
    Please send your support messages for the mission, or tweet it including the hashtag #HTV5.

    KOUNOTORI5 launch rescheduled to 8:50:49 p.m. on August 19 (Wed.) 2015

    Aug. 16, 2015 Updated
    KOUNOTORI5 launch postponed to Aug. 19 (Wed., JST)

    The launch date of the H-IIB Launch Vehicle No. 5 carrying the KOUNOTORI5 has been postponed as unfavorable weather is forecasted. The launch was originally scheduled for August 17. The live broadcast of the launch will also be put off accordingly.
    Your support messages are very much welcome through Twitter (Hashtag “#HTV5”) or via the following website.

    KOUNOTORI5 launch postponed to Aug. 19 (Wed., JST)

    Aug. 15, 2015 Updated
    New launch date and time of KOUNOTORI5/H-IIB F5 decided

    Aug. 14, 2015 Updated
    KOUNOTORI5 launch postponed to Aug. 17 (Mon., JST)

    The launch date of the H-IIB Launch Vehicle No. 5 carrying the KOUNOTORI5 has been postponed as unfavorable weather is forecasted. The launch was originally scheduled for August 16. The live broadcast of the launch will also be put off accordingly.
    Your support messages are very much welcome through Twitter (Hashtag “#HTV5”) or via the following website.

    KOUNOTORI5 launch postponed to Aug. 17 (Mon., JST)

    Jul. 21, 2015 Updated
    Dates set for capturing the KOUNOTORI5 and its berthing with ISS Astronaut Yui to be in charge of operation

    After international coordination, the dates for capturing the KOUNOTORI5, a cargo transporter to the International Space Station (ISS), and its berthing have been respectively set as August 20 (Thu.) and 21 (Fri.) The KOUNOTORI5 is scheduled to be launched on August 16 (Sun.) from the Tahegashima Space Center.
    It was also decided that Astronaut Kimiya Yui will manipulate the ISS robotic arm to capture the KOUNOTORI2.

    Dates set for capturing the KOUNOTORI5 and its berthing with ISS Astronaut Yui to be in charge of operation

    Jul. 10, 2015 Updated
    KOUNOTORI5 and operation simulation training opened to the press

    On July 1, the KOUNOTORI5, a cargo transporter to the ISS, was revealed to the media at the Tanegashima Space Center. The mission was also explained there.
    From the evening of July 9 to the morning of the 10th, simulation training for the KOUNOTORI5 operation and control was held in the KOUNOTORI operation room at the Tsukuba Space Center, and part of it was also open to the press. This training was a last opportunity for a joint session between JAXA and NASA before the KOUNOTORI5 launch. On the NASA side, Astronaut Wakata participated in the training as a CAPCOM (capsule/spacecraft communicator).

    KOUNOTORI5 and operation simulation training opened to the press

    Jun. 9, 2015 Updated
    Launch day set for KOUNOTORI5/H-IIB F5!

    The launch date and time for the H-IIB Launch Vehicle No. 5 (H-IIB F5) with the H-II Transfer Vehicle “KOUNOTORI5” (HTV5) onboard was set for around 10:01 p.m. on August 16 (Sun.), 2015 (Japan Standard Time).
    The H-IIB F5 has already been transported to the TNSC, and it is now being assembled there.
    * Launch time will be determined by the updated orbit of the ISS.

    Launch day set for KOUNOTORI5/H-IIB F5!

    Sep. 7, 2013 Updated
    KOUNOTORI4 completed its mission with re-entry!

    The KOUNOTORI4 (HTV4, a cargo transporter to the International Space Station) left the ISS on Sept. 5 and re-entered the atmosphere at 3:37 p.m. on Sept. 7 (Japan Standard Time.)
    The KOUNOTORI 4 successfully achieved its mission of taking cargo to the ISS, then completed all its tasks over about 36 days.
    We would like to send our sincere appreciation to all of you who have been supporting the KOUNOTORI project.

    KOUNOTORI4 completed its mission with re-entry!

    Sep. 3, 2013 Updated
    Re-entry date and time for KOUNOTORI4 decided

    Schedules of departure from the International Space Station (ISS) and of re-entry to the atmosphere for the H-II Transfer Vehicle “KOUNOTORI 4” (HTV4) are determined as follows.

    Departure from the ISS:
    September 5, 2013 / 1:00 a.m.(Japanese Standard Time, JST)*
    Re-entry to the atmosphere:
    September 7, 2013 / 3:36 p.m.(JST)*

    * The time may vary according to the actual operation.

    Aug. 10, 2013 Updated
    KOUNOTORI4 berthed at ISS!

    The KOUNOTORI4 (HTV4, a cargo transporter to the International Space Station) was captured by the ISS robotic arm at 8:22 p.m. on August 9 (Japan Standard Time) and berthed at the ISS at 3:38 a.m. on August 10 (JST). The KOUNOTORI4 was launched by the H-IIB Launch Vehicle No.4 on August 4. ISS astronauts will take cargo out from the Pressurized and Unpressurized Logistic Carriers into the ISS.

    Aug. 9, 2013 Updated
    Live broadcast of KOUNOTORI4 trip to ISS!

    The KOUNOTORI3 (HTV4, the cargo transporter to the International Space Station) launched on August 4 has been traveling to the ISS while adjusting its altitude. Between the evening on August 9 and early on the morning of August 10, the KOUNOTORI4 will make a final approach and berth at the ISS. JAXA will provide a live broadcast of its final access, capture, and berthing.
    The KOUNOTORI4’s approach and the ISS’s capture of the vehicle by the robotic arm is scheduled for about one hour from 7:40 p.m. on the 9th (Japan Standard Time.) Then the telecast of its berthing will last for about one hour from 22:00 p.m. on the 9th (JST.)
    Please don’t miss the broadcast!
    (Photo: The KOUNOTORI3 approaching the ISS, JAXA/NASA)

    Aug. 4, 2013 Updated
    Launch Success of KOUNOTORI4/H-IIB F4

    The H-IIB Launch Vehicle No. 4 with the KOUNOTORI4 (HTV4, a cargo transporter to the International Space Station) onboard lifted off from the Tanegashima Space Center at4:48:46 a.m. on August 4 (Sun., Japan Standard Time.)
    The launch vehicle flew smoothly, and at 14 minutes and 59 seconds after liftoff, the KOUNOTORI4 separation was confirmed.
    The KOUNOTORI4 will gradually go closer to the International Space Station, and it will be berthed at the ISS. We will broadcast the berthing on our website, so don’t miss it!

    Jun. 19, 2013 Updated
    KOUNOTORI4 revealed at TNSC

    On June 19, the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) “KOUNOTORI4” was shown to the media at the Tanegashima Space Center (TNSC.)
    The KOUNOTORI4 will be launched by the H-IIB Launch Vehicle No. 4 on Aug. 4 from the TNSC. It will carry various goods to the ISS including food and water for astronauts, as well as experiment devices and materials for the Japanese Experiment Module “Kibo.” Launch preparations continue for the KOUNOTORI4.

    May 21, 2013 Updated
    KOUNOTORI4/H-IIB F4 launch schedule decided!

    The H-IIB Launch Vehicle No. 4 (H-IIB F4) carrying the H-II Transfer Vehicle (HTV4, a cargo transporter to the International Space Station) will be launched on August 4 (Sunday, Japan Standard Time.) The launch time will be around 4:48 a.m. (JST.) It will be blasted off from the Yoshinobu Launch Complex at the Tanegahsima Space Center. Why don’t you take this opportunity to come to Tanegahima to witness the liftoff at hand!

    Sep. 14, 2012 Updated
    KOUNOTORI3 completed its mission with re-entry!

    The KOUNOTORI3 (HTV3, a cargo transporter to the International Space Station) left the ISS on Sept. 13 and re-entered the atmosphere at 2:27 p.m. on Sept. 14 (Japan Standard Time.)
    The KOUNOTORI 3 successfully achieved its mission of taking cargo to the ISS, then completed all its tasks over about 56 days.
    We would like to send our sincere appreciation to all of you who have been supporting the KOUNOTORI project.

    Sep. 11, 2012 Updated
    KOUNOTORI3 departure and re-entry live report!

    The H-II Transfer Vehicle “KOUNOTORI3” (HTV3,a cargo transporter to the International Space Station) will leave from the ISS at around 0:50 a.m. on Sept. 13 (Japan Standard Time, all the following dates and time are JST,) and will re-enter the atmosphere at around 2:24 p.m. on Sept. 14.
    JAXA will offer a live report of its departure from the ISS from 0:20 a.m. on the 13th (Thu.), then a live scene of the HTV operation room at the time of its re-entry from 1:45 p.m. on the 14th (Fri.) through the Internet. Please do not miss the footage!

    Sep. 7, 2012 Updated
    Re-entry date and time for KOUNOTORI3 decided

    The re-entry schedule for the KOUNOTORI3 was set as follows after extended mooring at the International Space Station due to an additional extravascular activity.

    Departure from the ISS:
    September 13, 2012 / 0:50 a.m.(Japanese Standard Time, JST)*
    Re-entry to the atmosphere:
    September 14, 2012 / 2:24 p.m.(JST)*

    * The time is subject to change due to actual operational status.

    The KOUNOTORI3 will carry a re-entry data recorder, the i-Ball, which was developed in cooperation between the public and private sectors to acquire atmosphere re-entry data as well as scenes of KOUNOTORI3’s destruction.

    Jul. 28, 2012 Updated
    KOUNOTORI3 berthed at ISS!

    The KOUNOTORI3 (HTV3, a cargo transporter to the International Space Station) was captured by the ISS robotic arm at 9:23 p.m. on July 27 (Japan Standard Time) and berthed at the ISS at 2:31 a.m. on July 28. The KOUNOTORI3 was launched by the H-IIB Launch Vehicle No.3 on July 21. ISS astronauts will take cargo out from the Pressurized and Unpressurized Logistic Carriers into the ISS.
    (Photo: The KOUNOTORI3 to a Common Berthing Mechanism at the nadir port of Harmony, JAXA/NASA)

    Jul. 21, 2012 Updated
    Launch Success of KOUNOTORI3/H-IIB F3

    The H-IIB Launch Vehicle No. 3 with the KOUNOTORI3 (HTV3, a cargo transporter to the International Space Station) onboard lifted off from the Tanegashima Space Center at 11:06:18 on July 21 (Sat., Japan Standard Time.)
    The launch vehicle flew smoothly, and at 14 minutes and 53 seconds after liftoff, the KOUNOTORI3 separation was confirmed.
    The KOUNOTORI3 will gradually go closer to the International Space Station, and it will be berthed at the ISS. We will broadcast the berthing on our website, so don’t miss it!

    Jun. 21, 2012 Updated
    KOUNOTORI3/H-IIB F3 Special Site now open!

    JAXA will launch the KOUNOTORI3 (a cargo transporter to the International Space Station, ISS) by H-IIB Launch vehicle No.3 on July 21 from the Tanegashima Space Center. We have opened the KOUNOTORI3/H-IIB F3 Special Site to be ready for the launch.
    Please check the special site for more information. We have also started welcoming your support messages, so please send them to us!

    Jun. 7, 2012 Updated
    KOUNOTORI3 revealed to the media at TNSC

    On June 1 (Fri.), the H-II Transfer Vehicle “KOUNOTORI3” (HTV3, a cargo transporter to the International Space Station) was revealed to the media at the Spacecraft and Fairing Assembly Building 2 at the Tanegashima Space Center. The KOUNOTORI3 will be packed with food and daily necessities for astronauts aboard the ISS, test equipment for aquatic organisms, and other experiment devices including a small satellite, then will be launched by the H-IIB Launch Vehicle No. 3 at 11:18 a.m. on July 21, 2012 (Japan Standard Time.) The KOUNOTORI is currently under preparations for its journey to space.

    Mar. 21, 2012 Updated
    KOUNOTORI3/H-IIB F3 launch schedule decided!

    The launch date and time for the H-IIB Launch Vehicle No. 3 (H-IIB F3) with the H-II Transfer Vehicle “KOUNOTORI3” (HTV3), a cargo transporter to the International Space Station, has been set to be at around 11:18 a.m. on July 21 (Sat.), 2012 (Japan Standard Time.) The launch preparation operation for the KOUNOTORI is smoothly in progress at the Tanegashima Space Center.

    Mar. 30, 2011 Updated
    KOUNOTORI2 re-entered the atmosphere to complete its mission!

    The KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station,) which left the ISS at around 0:46 a.m. on March 29 (Japan Standard Time,) re-entered the atmosphere at around 12:09 p.m. on March 30 (JST.)
    The KOUNOTORI2 successfully completed its role to transport materials to the ISS, then re-entered the Earth’s atmosphere to complete its mission of approximately 67 days.
    Thank you very much for supporting the KOUNOTORI2 and H-IIB Launch Vehicle No.2 missions.

    Mar. 29, 2011 Updated
    KOUNOTORI2 left ISS!

    The KOUNOTORI2 (HTV2, a cargo transporter to the ISS) was detached from the International Space Station (ISS) using the ISS robotic arm at 10:29 p.m. on March 28 (Japan Standard time,) and it emitted a jet to leave the ISS after being transported to the release point at 0:46 a.m. on the 30th.
    The KOUNOTORI2 will re-enter the Earth’s atmosphere at around 12:09 on March 30. From some areas, you can see the KOUNOTORI2 flying around the Earth between the 29th and the 30th. Also, please witness the scene of the HTV operation and control room when it re-enters the atmosphere through the live Internet broadcast, which will begin at 11:30 a.m. on the 30th.

    Mar. 25, 2011 Updated
    KOUNOTORI2 leaving ISS on the 29th! Live broadcast scheduled

    The KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station) will depart from the ISS with used material loaded on March 29 (Japan Standard Time,) and will be slated for re-entry to the atmosphere on the 30th (JST.) JAXA will broadcast a live Internet report of the KOUNOTORI departure from the ISS from 0:00 a.m. on the 29th (JST,) then its re-entry to the atmosphere from 11:30 a.m. on the 30th (JST.) Please watch the events through the Internet!

    Mar. 22, 2011 Updated
    KOUNOTORI2 to leave ISS

    The departure date of the KOUNOTORI2 (HTV2, a cargo transporter to the ISS), which is loaded with used materials, from the International Space Station (ISS) has been decided.
    The KOUNOTORI2 will leave the ISS at around 0:45 a.m. on March 29 (Japan Standard Time) after completing its role at the ISS. After departure, it will be burned when it re-enters the atmosphere at around 12:10 p.m. on March 30. Following its combustion, its mission will be accomplished.
    We will broadcast a live report of the departure and re-entry of the KOUNOTORI2. More details will be posted on our website. (Photo by NASA)

    Mar. 11, 2011 Updated
    KOUNOTORI2 relocation to the earth-facing port completed

    At 8:49 p.m. on March 10 (Japan Standard Time), the KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station) began to be moved from the zenith port to the earth-facing port using the robotic arm of the International Space Station. At 3:55 a.m. on the 11th (JST,) KOUNOTORI2’s electric and communication systems were connected to the ISS to complete the relocation. After being loaded with used items, the KOUNOTORI2 will re-enter the atmosphere to be burned.

    Mar. 9, 2011 Updated
    KOUNOTORI2 to return to earth-facing port from March 10

    The KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station), will move back to the earth-facing port of the Harmony (Node 2) from its zenith port now that the Space Shuttle Discovery left the ISS to go home on March 7 (Japan Standard Time.) The relocation is scheduled to be performed on the 10th and 11th (JST.) More cargo will be taken out of the KOUNOTORI2, then, after being packed with used materials, the KOUNOTORI2 will re-enter the atmosphere.
    (Photo by NASA)

    Feb. 21, 2011 Updated
    KOUNOTORI2 relocation to the zenith port completed

    As part of preparations for the Space Shuttle Discovery’ s docking with the International Space Station (ISS,) the KOUNOTORI2 , or the HTV2, a cargo transporter to the ISS, was moved from the earth-facing port of the Harmony (Node 2) to its zenith port. This was the first time to perform such a relocation. The KOUNOTORI2 was successfully transported at 1:45 a.m. on Feb. 19 (Japan Standard Time,) and the electric cables were connected with the Harmony at 4:26 a.m. (JST) to complete its relocation.

    Jan. 28, 2011 Updated
    KOUNOTORI2 berthing at ISS

    The KOUNOTORI2, or the HTV2, a cargo transporter to the International Space Station (ISS) launched by the H-IIB Launch Vehicle No.2, was captured by the ISS robotic arm at around 8:41 p.m. on January 27 (Japan Standard Time,) and, at around 3:34 a.m. on the 28th (JST,) the KOUNOTORI berthed at the ISS. Cargo in the Pressurized Section will be transported to the ISS by the ISS astronauts followed by cargo in unpressurized areas.

    Jan. 22, 2011 Updated
    KOUNOTORI2/H-IIB F2 successfully launched

    The H-IIB Launch Vehicle No. 2 with the KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station, ISS) onboard was launched from the Tanegashima Space Center at 2:37:57 p.m. on January 22 (Sat., Japan Standard Time.) The launch vehicle flew smoothly, and, at about 15 minutes and 13 seconds after liftoff, the separation of the KOUNOTORI2 was confirmed.
    The KOUNOTORI2 will fly to the ISS, then, on Jan. 28 (Fri., JST,) it is slated for berthing with the ISS.

    Dec. 14, 2010 Updated
    KOUNOTORI2 system checkup completed

    At the Tanegashima Space Center, all parts of the H-II Transfer Vehicle “KOUNOTORI2” (HTV2) were integrated electrically and mechanically in the end of October. Throughout November, the assembled KOUNOTORI2 has been checked as one system to confirm that no problem was found in the vehicle.
    After a thorough inspection, propellants were loaded onto the KOUNOTORI2 tanks, and currently the tank pressure is being adjusted. Preparation for launch is smoothly progressing.
    The final launch preparation including battery charge and loading onto the H-IIA Launch Vehicle No.2 will now be carried out for the KOUNOTORI2.

    Dec. 1, 2010 Updated
    KOUNOTORI2 control and operation simulation revealed to the press

    On November 30, JAXA showed part of the control and operation simulation of the KOUNOTORI2 to the media at the Tsukuba Space Center. The KOUNOTORI2 (HTV2) is a cargo transfer vehicle to the International Space Station (ISS.)
    The purpose of the simulation was to train and improve operators’ skills. It takes about 20 hours with NASA to simulate events, from the KOUNOTORI2’s arrival at around 12-km beneath the ISS, to its gradual approach to the ISS, to the capture of the KOUNOTORI2 by the ISS robotic arm, and then the docking of the KOUNOTORI2.

    Nov. 26, 2010 Updated
    KOUNOTORI2 shown to the Press at TNSC

    On Nov. 25, the H-II Transfer Vehicle “KOUNOTORI”2 (a cargo transporter to the International Space Station) was revealed to the media at the Spacecraft and Fairing Assembly Building No. 2 at the Tanegashima Space Center. We are engaging in preparation for the launch of the KOUNOTORI2 including propellant loading and mating with the launch vehicle.
    JAXA provides updated information about the KOUNOTORI2 and H-IIB Launch Vehicle No.2 at the special site. Your support messages are welcome there, too.

    Nov. 11, 2010 Updated
    HTV nickname selected & special site open!

    “KOUNOTORI” (meaning “a white stork” in English) was chosen as the nickname of the H-II Transfer Vehicle (HTV, a cargo transfer vehicle to the International Space Station.)
    During a month-long nickname campaign, we received 17,236 suggestions.
    Among them, “KOUNOTORI” was selected because a white stork carries an image of conveying an important thing (a baby, happiness, and other joyful things); therefore, it precisely expresses the mission to transport essential materials to the ISS.
    The KOUNOTORI2 is scheduled to be launched by the H-IIB Launch Vehicle No. 2 (H-IIB F2) at around 3:29 p.m. (Japan Standard Time) on January 20 (Thu.), 2011.
    Taking this opportunity of selecting the nickname, we would also like to open the “KOUNOTORI2/H-IIB F2 Special Site.” We will provide you with updated information about the project including a column by project personnel and launch related matters. Please enjoy the site!
    * Launch time will be determined by the updated orbit of the ISS.

    Nov. 10, 2010 Updated
    Launch day set for HTV2/H-IIB F2!

    The launch date and time for the H-IIB Launch Vehicle No. 2 (H-IIB F2) with the H-II Transfer Vehicle (HTV2) onboard was set for around 3:29 p.m. on January 20 (Thu.), 2011 (Japan Standard Time). The HTV2 is a cargo transporter to the International Space Station (ISS.) The integration of all modules of the HTV2 was completed at the Tanegashima Space Center (TNSC), and it will enter the final launch preparation phase. The H-IIB F2 has already been transported to the TNSC, and it is now being assembled there.
    * Launch time will be determined by the updated orbit of the ISS.

    Nov. 2, 2010 Updated
    HTV2: all modules connected, moved to final launch preparations

    (Left) All HTV2 modules are being connected (Center) Integrated HTV2 (front side) (Right) Integrated HTV2 (back side) (Images by JAXA)

    On Oct. 29, we completed connecting all modules of the second H-II Transfer Vehicle (HTV2, a cargo transporter to the International Space Station) electrically and mechanically at the Second Spacecraft and Fairing Assembly Building (SFA2) at the Tanegashima Space Center. The HTV2 is now in its configuration for launch.
    After a comprehensive check on the integrated HTV2, it will go through final launch preparations including propellant loading and fairing encapsulation. The HTV2 is scheduled to be launched in the winter launch period of Japan Fiscal Year 2010.

    Oct. 13, 2010 Updated
    Full assembly started for the second HTV

    The assembly operation for all modules of the second H-II Transfer Vehicle (HTV, the cargo transporter to the International Space Station) started on October 6 at the second Spacecraft and Fairing Assembly Building (SFA2) at the Tanegashima Space Center. Prior to full assembly, in mid September, cargo to the ISS was loaded onto the Pressurized and Unpressurized Carriers.

    Apr. 7, 2010 Updated
    Development of HTV/H-IIB received Japan industry technology/MEXT award

    JAXA was selected as one of 12 organizations to receive the Ministry of Education, Culture, Sports, Science and Technology award at the 39th Japan industry technology awards for its development of the HTV and H-IIB launch vehicle.
    The Japan industry technology awards are presented by Nikkan Kogyo Shimbun Ltd. (Business and Technology Daily News, Japan) to encourage development of original and unique technology that contributes to the promotion of industry. The news company bestows the awards to development projects of distinctive large-scale technological systems.

    Feb. 10, 2010 Updated
    HTV Project Team awarded for research

    Since 2005, the National Institute of Science Technology Policy (NISTEP) of the Ministry of Education, Culture, Sports, Science and Technology (MEXT) has been choosing researchers who have made significant contributions to science and technology every year to praise their efforts. In 2009, the demonstration flight of the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) was highly evaluated, and on February 9, Mr. Torano, HTV Project Manager, Mr. Koyari, Sub-project Manager, and Mr. Sasaki, Functional Manager, received a memento of the selection.

    Nov. 2, 2009 Updated
    HTV re-entered the atmosphere, mission completed

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which departed from the International Space Station (ISS) on October 31, re-entered the atmosphere at around 6:26 a.m. on November 2.
    The HTV successfully completed its cargo transportation operations to the ISS, and accomplished all its missions in about 52 days following the re-entry today.

    Oct. 31, 2009 Updated
    HTV released from ISS

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which completed its cargo transportation mission at the International Space Station (ISS), was unberthed from the ISS by its robotic arm (SSRMS) at 0:02 a.m. on October 31 (Japan Standard Time, the following dates and times are JST.) The HTV departed from the ISS at 2:32 a.m. on the 31st. The HTV will leave the ISS orbit, and is scheduled to re-enter the Earth’s atmosphere at around 6:25 a.m. on November 2 (Mon.)
    You may be able to see the HTV just prior to re-entry from Okinawa at around 6:13 a.m. on the 2nd if the deorbit process goes smoothly and the weather cooperates. (Photo by NASA)

    Oct. 27, 2009 Updated
    Internet Live Report: HTV leaving ISS on Oct. 31 (Sat)

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which is currently berthed at the International Space Station (ISS), is scheduled to depart from the ISS at 2:30 a.m. on Oct. 31 (Sat) (Japan Standard Time, all the following days and times are in JST.) The HTV will be unberthed from the ISS by the ISS robotic arm (SSRMS) late at night on Oct. 30 (Fri) after its hatch to the ISS is closed at dawn of Oct. 30, then depart from the ISS. If everything goes smoothly, the HTV will re-enter the Earth’s atmosphere around 6:25 a.m. on Nov. 2 (Mon).

    We will broadcast a live report of the HTV unberthing and departure from the ISS through the Internet from 11:45 p.m. on Oct. 30 (Fri) and from 2:15 a.m. on Oct. 31 (Sat) respectively. (Sorry, the live reports are broadcasted only in the Japanese language.) Please enjoy the HTV live reports over the weekend!
    The live broadcast time schedule has changed due to the delay of the HTV departure.

    Oct. 21, 2009 Updated
    The HTV PLC unloading operations completed, trash loading continues

    HTV-1, being berthed to the ISS, is operating nominally. The Small Fine Arm (SFA) of the Kibo Remote Manipulator System (JEMRMS), packed in a Cargo Transfer Bag (CTB) and delivered to the ISS, was transferred from the HTV Pressurized Logistics Carrier (PLC) to Kibo on October 4. The Pressurized Stowage Resupply Rack (PSRR), also delivered on the HTV-1, was transferred to Kibo’s Experiment Logistics Module-Pressurized Section (ELM-PS) on October 14. All the cargo transfer operation from the HTV PLC to the ISS was completed on October 20.
    Aboard the ISS, trash loading into the HTV PLC is currently underway. With this trash stow activity completed, the HTV-1 will depart from the ISS, and enter the atmosphere early next month.
    Photo (provided by NASA): Astronaut Robert Thirsk taking cargo out from the HTV Pressurized Carrier.

    Oct. 14, 2009 Updated
    HTV operations running smoothly, cargo unloading continues

    Cargo unloading operations continued from the Pressurized Logistics Carrier of the H-II Transfer Vehicle (HTV) Demonstration Flight berthed at the International Space Station (ISS). On Oct. 4, the Small Fine Arm (SFA) of the Kibo’s Robotic Arm was moved to the ISS. The SFA was transported to the ISS as it was still packed in the Cargo Transfer Bag. One unit of the Pressurized Stowage Resupply Rack will be transferred to the ISS on the 14th.
    Photo (provided by NASA): Astronaut Nicole Stott taking cargo out from the HTV Pressurized Carrier.

    Sep. 26, 2009 Updated
    Exposed Pallet stored back in HTV

    The Exposed Pallet of the H-II Transfer Vehicle (HTV) Demonstration Flight was retrieved and stored back in the HTV Unpressurized Carrier at 10:20 p.m. on Sept. 25 (Japan Standard Time) by the robotic arms of the Kibo and the International Space Station (SSRMS) after its two cargoes, the experiment devices in the unpressurized environment, had been installed in the Kibo’s Exposed Facility.
    Cargo in the HTV Pressurized Carrier will now be unloaded by the astronauts aboard the ISS. After the unloading, used material and equipment on the ISS will be packed into the Pressurized Carrier. The HTV will depart from the ISS in mid-November to re-enter the atmosphere. (The detailed schedule will be decided based on the ISS/HTV operational status.) (Photo by NASA)

    Sep. 25, 2009 Updated
    Two experiment devices installed onto Kibo Exposed Facility

    On Sept. 24 and 25 (Japan Standard Time), two experiment devices that were shipped by the H-II Transfer Vehicle (HTV) Demonstration Flight were unloaded from the HTV Exposed Pallet and installed onto the Exposed Facility of the Japanese Experiment Module “Kibo.”
    The two devices are the “Superconducting Submilimeter-Wave Limb-Emission Sounder (SMILES)” and the “Hyperspectral Imager for the Coastal Ocean (HICO) & Remote Atmospheric & Ionospheric Detection System (RAIDS) Experimental Payload (HREP.)” The HREP and the SMILES were mounted at 8:15 p.m. on the 24th and 1:12 a.m on the 25th respectively. (Photo by NASA)

    Sep. 24, 2009 Updated
    HTV Exposed Pallet attached to the Kibo Exposed Facility

    At 6:06 p.m. on Sept. 23rd (Japan Standard Time, JST), the Exposed Pallet was taken out from the H-II Transfer Vehicle (HTV) Demonstration Flight, which is now berthed at the International Space Station (ISS). The Pallet was then attached onto the Exposed Facility of the Japanese Experiment Module “Kibo” at 11:33 p.m. (JST). The experiment devices on the Pallet will be moved to be installed onto the Kibo’s Exposed Facility. (Photo by NASA)

    Sep. 18, 2009 Updated
    HTV Demonstration Flight successfully berthed at ISS

    The H-II Transfer Vehicle (HTV) Demonstration Flight, launched by the H-IIB Launch Vehicle Test Flight at 2:01 a.m. on Sept. 11 (Japan Standard Time, JST,) took almost one week to approach the International Space Station (ISS) and arrived at the Berthing Point 10 meters below the ISS at 4:27 a.m. on the 18th (JST, following times are all JST.) At 4:51 a.m., the HTV was captured by the ISS robotic arm (Space Station Remote Manipulator System, SSRMS) manipulated by the ISS crew, and it was installed onto the Common Berthing Mechanism (CBM) on the lower side (earth side) of the Harmony (Node 2) at 7:26 a.m. At 10:49 a.m., electric and communication lines were connected, and the HTV was successfully berthed at the ISS.

    Sep. 15, 2009 Updated
    Live reports of the HTV final approach to the ISS on Sept. 18 (Fri.)

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which was launched by the H-IIB Launch Vehicle at 2:01:46 a.m. on September 11 (Fri.) has been smoothly flying on its scheduled course. Its final approach to the International Space Station (ISS) was approved at the ISS Mission Management Team (IMMT) meeting on Sept. 15, thus, from the 16th, the altitude of the HTV will be maneuvered to gradually approach the ISS. The HTV is scheduled to be berthed at the ISS on Sept. 18 (Fri.)
    JAXA will broadcast the live reports of the ISS robotic arm capturing the HTV from 4:00 a.m., and the berthing of the HTV at the ISS from 7:00 a.m. They are early in the morning, but don’t miss them!

    Sep. 11, 2009 Updated
    HTV/H-IIB Successfully Launched!!

    The Japan Aerospace Exploration Agency (JAXA) launched the H-II Transfer Vehicle (HTV) Demonstration Flight aboard the H-IIB Launch Vehicle Test Flight (H-IIB TF1) at 2:01:46 a.m. on September 11, 2009 (Japan Standard Time, JST) from the Tanegashima Space Center. The launch vehicle flew smoothly, and, at about 15 minutes and 6 seconds after liftoff, the separation of the HTV Demonstration Flight was confirmed.

    The HTV will gradually approach the International Space Station (ISS) and berth at the ISS on the 18th (Friday, JST.)

    Aug. 31, 2009 Updated
    HTV moved to the VAB! Final launch preparation phase

    On August 30, the encapsulated HTV Demonstration Flight was transported to the Vehicle Assembly Building (VAB.) It will be loaded onto the H-IIB Launch Vehicle to be ready for the launch on September 11. We published a promotion movie of the HTV/H-IIB mission. Please watch it before witnessing the actual launch!

    Aug. 24, 2009 Updated
    HTV encapsulated

    On August 21, the H-II Transfer Vehicle (HTV) Demonstration Flight was mated with the Payload Attach Fitting (PAF) at the Spacecraft and Fairing Assembly Building #2.
    On the 23rd, the HTV on the PAF was encapsulated by the payload fairing, which covers the payload to protect it from air resistance, friction and the acoustic vibrations of launch. The fairing for the HTV is a 5S-H type and is about 5 meters in diameter and about 15 meters in length. It was developed for the HTV launch.
    The encapsulated HTV Demonstration Flight will be transported to the Vehicle Assembly Building (VAB) and loaded onto the H-IIB Launch Vehicle Test Flight.

    Jul. 9, 2009 Updated
    HTV opened to the press at TNSC

    On July 9, the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) was opened to the press at the Spacecraft and Fairing Assembly Building #2 (SFA2) at the Tanegashima Space Center (TNSC.)
    We are providing updated information on the HTV and H-IIB at the HTV/H-IIB Special Site.

    Jul. 8, 2009 Updated
    HTV/H-IIB launch date decided! Special site opened

    The H-IIB Launch Vehicle Test Flight with the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) will be launched at 2:04 a.m. on September 11 (Fri.). (*)
    The HTV has been fully assembled at the Tanegashima Space Center, and it will be under final launch preparations including comprehensive checkout and propellant loading to be ready for launch.
    The ground comprehensive test for the H-IIB Launch Vehicle using the Ground Test Vehicle (the GTV test) is scheduled on the 11th.
    Please check the updated information on the HTV and H-IIB at the “HTV/H-IIB Special Site,” which was opened today. We hope you enjoy the site.
    (*) Time will be determined by the updated orbit of the International Space Station (ISS.)

    Jun. 30, 2009 Updated
    Preparations for the HTV Demonstration Flight going smoothly at TNSC

    Preparations for the Demonstration Flight of the H-II Transfer Vehicle (HTV) are underway at the Tanegashima Space Center (TNSC).
    At dawn on April 23, the HTV arrived at the TNSC and was moved into the Spacecraft and Fairing Assembly Building #2 for a post-transportation inspection on each element of the vehicle.
    Payloads to be shipped to the International Space Station (ISS) by the HTV were then loaded onto the HTV’s Pressurized Logistic Carrier and Unpressurized Logistic Carrier.

    In the Pressurized Logistic Carrier, life-related supplies, such as food and clothes, which were packed in the Cargo Transfer Bag (CTB) and other experiment materials were stored on the HTV Re-supply Rack (HRR) of the Carrier. In the Unpressurized Logistic Carrier, the Superconducting Submilimeter-Wave Limb-Emission Sounder (SMILES,) which is an experiment device for the Kibo’s Exposed Facility, and NASA experimental equipment were loaded onto the Exposed Pallet of the Carrier.

    After completing the payload loading, the two carriers were mated.
    On June 24, all HTV modules including the Avionics Module and Propulsion Module were connected.
    The HTV demonstration flight is now fully assembled, and will start final launch preparations such as a comprehensive vehicle inspection and propellant loading.

    Apr. 24, 2009 Updated
    HTV arrives at TNSC

    At dawn on April 23, the First H-II Transfer Vehicle (HTV) was transported from Shimama Port at Tanegashima to the Tanegashima Space Center (TNSC.) The HTV left the Tsukuba Space Center on April 17. The Pressurized Logistic Carrier, Unpressurized Logistic Carrier, the Avionics Module, and the Propulsion Module were detached for the transportation, thus they will be assembled after arrival. A final functional checkup will be held prior to the launch.

    Apr. 17, 2009 Updated
    HTV left for the TNSC

    The first H-II Transfer Vehicle (HTV), or the HTV Technology Demonstrator, left the Tsukuba Space Center at dawn on April 17, 2009, for the Tanegashima Space Center (TNSC.) After arrival, the HTV will be assembled and checked for launch by the H-IIB Launch Vehicle, which is now under testing.


    The first HTV leaving the TKSC (Unpressurized Logistics Carrier, Avionics Module, and Plopulsion Module)

    The first HTV arrived at Tsuchiura Port
    (Unpressurized Logistics Carrier)

    Dec. 26, 2008 Updated
    HTV open to the press

    On Dec. 25, 2008, JAXA revealed the maiden H-II Transfer Vehicle (HTV), an unmanned supply transfer vehicle that will fly to the International Space Station (ISS), to the press at the Tsukuba Space Center (TKSC.) It was the first press conference since assembling all the modules of the first HTV.

    At the press conference, the HTV and its launch by the H-IIB Launch Vehicle were explained by HTV Project Manager Yoshihiko Torano and H-IIB Launch Vehicle Project Manger Tomihisa Nakamura. The Superconducting Submilimeter-Wave Limb-Emission Sounder (SMILES,) which will be transported to the ISS by the first HTV, was also introduced by Professor Masato Shiotani of the Research Institute for Sustainable Humanosphere of Kyoto University. The SMILES is one of the experiment devices that will be installed onto the Exposed Facility of the Japanese Experiment Module “Kibo.”

    Also at the press conference, the first HTV and the SMILES undergoing an all-vehicle functional test were shown to the media at the Spacecraft Integration and Test Building at the TKSC. The modules of the cargo section (“Pressurized Carrier” and “Unpressurized Carrier,”) “Avionics Module” and “Propulsion Module” were assembled for the test. The “Exposed Pallet” loaded with a dummy cargo for the test and the SMILES were also displayed.

    We will conduct comprehensive functional tests with the mechanically and electrically integrated HTV, such as conductivity verification of the pipes and electric system, and other compatibility tests. The HTV is then scheduled to be transported to the Tanegashima Space Center in April, 2009, at the earliest, and be launched by the H-IIB Launch Vehicle in the summer launch season of 2009 or later.

    Dec. 18, 2008 Updated
    All flight modules assembled for first time for inaugural HTV flight

    On Dec. 12, all the parts of the H-II Transfer Vehicle (HTV,) the supply transfer vehicle to the International Space Station, were assembled for an all-vehicle functional test ahead of its first flight. They are the “Logistic Carrier Pressurized Section,” the cargo section of the “Un-pressurized Carrier,” the “Exposed Pallet,” the “Avionics Module” and the “Propellant Module.” This was the first time that all the modules were assembled. The size of the assembled HTV was about the same size as the Pressurized Module of the Japanese Experiment Module “Kibo.” The HTV will be the largest payload that JAXA has ever launched.

    During the all-vehicle functional test, all the modules are mechanically and electrically connected to verify their function as one piece of the vehicle such as proper pipe routing and electric conductivity.

    The first HTV is scheduled to be launched by the H-IIB Launch Vehicle in September 2009 at the earliest.

    Aug. 28, 2008 Updated
    Thermal Vacuum Test for first flight of HTV

    A thermal vacuum test on the first flight vehicle of the H-II Transfer Vehicle (HTV) has been carried out at the Spacecraft Integration and Test Building at the Tsukuba Space Center.
    The purpose of the test is to evaluate the thermal design of the structure and to verify its endurance in the harsh environment of space by simulating the vacuum and thermal environment in space.
    Thermal vacuum tests for the Pressurized Carrier and Unpressurized Carrier have already been completed, and the main part with the Avionics Module and Propulsion Module combined is now in the 13-meter diameter space chamber for testing.
    The test will be completed in early September before the acoustic test and functional test are performed. After all the test results are reviewed to make sure that no problem is left unsolved, the vehicle will be transported to the Tanegashima Space Center for final launch preparations.

    (Photo: The main part of the HTV (Avionics Module and Propulsion Module) moved into the 13-meter diameter space chamber)

    Apr. 18, 2008 Updated
    The first model HTV (Technology Demonstration Model) was shown to the press

    On April 17, 2008, a press review was held for the first model H-II Transfer Vehicle (HTV) (Technology Demonstration Model), which is an unmanned cargo transfer spacecraft to the International Space Station. On display separately were the Pressurized Logistics Carrier for supply transportation, the Avionics Module for vehicle body control and the Propulsion Module which carries the propulsion system. When the HTV is completed and fully equipped, it will be the largest spacecraft in Japan with a length of 10 meters and a weight of 16.5 tons. After going through performance tests like the Thermal Vacuum Test and Acoustic Test, the first model HTV is scheduled for launch from Tanegashima on the H-IIB Launch Vehicle No. 1 (Test Model) in the summer of 2009.

    Jul. 2, 2007 Updated
    Proximity Communication System (PROX) undergoes testing

    Tests are currently being performed on the Proximity Communication System (PROX) at NASA’s Kennedy Space Center (KSC).

    The PROX system will be installed in the Japanese Experiment Module “Kibo” to communicate between the H-II Transfer Vehicle (HTV) and transmit and receive data between the International Space Station (ISS). It will also measure the relative distance and speed between the ISS and the HTV in order to support the HTV’s rendezvous with the ISS.

    Since last year, tests on the PROX and a compatibility test for the PROX/rack had been carried out before it went through a pre-shipping examination and was shipped out to the U.S. in January 2007. After performing several tests like the JEM/PROX compatibility test, it will be installed in the Experiment Logistics Module Pressurized Section (ELM-PS) and is scheduled for launch on Assembly Flight 1J/A at the end of February 2008.

    Photo1 : A general view of the PROX (Bottom right is the PROX before shipping at Tsukuba Space Center).
    Photo2 : A scene from a test on the PROX at the Kennedy Space Center.
    Photo3 : A crew review scene performed by astronaut Furukawa (taken from behind the PROX rack.)

    Jun. 26, 2006 Updated
    Prototype HTV unveiled to press at Tsukuba Space Center

    On June 23, a prototype of the H-II Transfer Vehicle (HTV) was unveiled to the press at the Tsukuba Space Center (TKSC.) The HTV is an unmanned orbital carrier to the International Space Station (ISS.) It is equipped with both the function of a “manned cargo carrier” for ISS crews to actually embark and carry out supportive work on it and the function of an “inter-orbital carrier” to perform “inter-orbit transportation to a selected attitude,” “rendezvous flights to the ISS,” and “re-entry” to aim to acquire the necessary technology for autonomous activities in space.

    The prototype will be used for various environment tests to make sure it can bear the extreme temperatures in space and acoustic and vibration environment at the time of launch. Through the tests, the project team will verify basic design data, and incorporate test results into future development.

    Outline of the HTV project

    Length about 10 m (including thruster)
    Diameter about 4.4 m
    Mass about 10.5 ton (excluding cargo)
    Loading capacity (for supply) about 6 tons
    Loading capacity (for waste) about 6 tons
    • Target orbit: ISS orbit
      Altitude: 350 to 460 km
      Inclination: about 51.6 degrees
    • Mission hours
      Solo flight: about 100 hours
      Stand-by: more than a week
      Docked with the ISS: about 30 days

    May 28, 2004 Updated
    Debris protection function was verified by shooting aluminum balls at the HTV at 6 km per second.

    Each module of the Space Station including the Japan Experiment Module has a “debris bumper” for protecting itself from losing its functions by colliding with space debris.
    The level of protection depends on the location (position) of each module and the probability of collision. Many technological ideas are incorporated to achieve the required protection effect, such as making the distance between the debris bumper and the pressurized wall longer.
    Solar array panels around the HTV have been considered to be part of the protective walls, but they needed to be verified.
    The verification was performed by a high-speed collision test using a HTV mockup. Aluminum balls of various sizes were shot at the protective walls at a speed of 6 km per second. After the test, the pressurized wall behind the protective walls was checked for holes. As a result, the solar array panels and the panel structure (an aluminum honeycomb structure) were verified to be effective for protection, and necessary data were also acquired for the further debris protection design assessment for the HTV.

    Upper Photo: A mockup for the verification (The thick wall on the right is a solar array panel.)
    Lower Photo:A solar panel from the back after the verification.

    Upper Photo: A mockup for the verification (The thick wall on the right is a solar array panel.)/Lower Photo:A solar panel from the back after the verification.;

    Mar. 28, 2003 Updated
    Manufacturing “Thermal Structural Test Models ” for Tests in the Next Fiscal Year

    HTV is about four meters in diameter and a bit shorter than 10 meters in length. In other words, its size can be explained as a container that could accommodate a sightseeing bus. In the process of developing HTV, therefore, it is divided into four modules namely Logistic Carrier Pressurized section, Logistic Carrier Un-Pressurized section, Avionics module, and Propulsion module. Thermal structural test models are being manufactured for each module. A thermal structural test model is a mimic model to test it in simulated harsh launch and space environments for checking acoustic condition, vibration, shock at separation and endurance in the space.

    The main structure is in conical semi-monocoque structure based on a launch vehicle design, and four modules will be assembled at the final fabrication phase and be tested for evaluating comprehensive strength and stiffness.

    Furthermore, tests for evaluating strength, pressure, acoustic data, shock, and heat balance, and acquisition of resonance frequency will be carried out to collect data for specifying environmental conditions of onboard loads and to find environmental characteristics data. The series of these tests will start in the next fiscal year.

    Upper Photo: Structural Thermal Test Model for Main Structure
    Lower Photo: Thermal Structural Test Model for Propulsion System “Helium Gas Supply Sub-Module”

    Oct. 5, 2001 Updated

    After HTV’s arrival to International Space Station (ISS), Exposed Pallet is taken out of HTV, and cargoes are replaced by robotic arm. This Exposed Pallet has rollers on its sides to minimize the friction and to keep the position accurately when it is brought back to HTV.
    A series of roller rotation slip tests was conducted from August to September 2001. The rollers are made of plastic to reduce the weight and they have solid lubricant on their surfaces. This combination of plastic and solid lubricant is rare. The purpose of this test is to confirm the manufacturing process and to collect the basic data of friction in the various environments (hot, cold, vacuum, air) and the wearing life.
    In addition, by conducting the test with the full-size model, the friction data closer to the actual operation were collected. The data will be applied not only for the HTV design and robotics analysis but also the future satellite programs and space equipment.

    Upper Photo: Setup for the rotation test in vacuum heat chamber
    Lower Photo: Setup for the full-size roller test

    Jun. 29, 2001 Updated

    Post Development Review of HTV Pressurized Carrier Aft Dome
    NASDA conducted additional preliminary design review (delta-PDR) with lots of participant from NASA and CSA (including ISS program manager) at Tsukuba Space Center as following schedule.
    Pre-Board Meeting : May 15th and 16th, 2001
    Board Meeting : May 18th, 2001
    We focused on two kinds of items in this review panel. One was a kind of additional items which were not reviewed in PDR held in 1999 (e.g.Un-pressurized carrier / Exposed pallet, GPS receivers in JEM, Crew operation panel, etc.) and another was a kind of items which had been changed the design from PDR (e.g. Solar power generation system, Approaching trajectory, etc.).
    Prior to holding the review panel, NASDA delivered review documents toward NASA, CSA and ESA and received a thousand of “Review Item Disposition Sheets (RID)” on these documents. We determined all dispositions for these RIDs after the discussions within three weeks. NASDA/NASA/CSA founded a few issues related to the ISS safety in this review panel and we determined to give high priority to these issues.

    Photo: HTV Delta-PDR Pre-Board Panel

    Feb. 19, 2001 Updated

    Post Development Review of HTV Pressurized Carrier Aft Dome A pressurized carrier equipped in HTV was designed based on the JEM Experiment Logistics Module Pressurized Section (ELM-PS). NASDA determined to use a newly designed integral molded structure for the Aft Dome of pressurized carrier to reduce the weight of 260 kg and the similar structure has already been used by the propellant tanks of Launch vehicles. Similar to H-IIA rocket, MAN-Technologie in Germany took the charge of the development under the supervision of Mitsubishi Heavy Industries LTD. Through this development, MAN-Technologie cleared the manufacturing problems such as thickness, welding, strength, etc., and completed them successfully. The photo shows a manufacturing sample that will be used for following engineering tests in Japan. After this review, NASDA will start manufacturing of the Flight Model and mass production.

    Photo: Aft Dome Structure for HTV Pressurized Carrier Engineering Test

    Dec. 8, 2000 Updated

    Succeeding to the previous tests conducted from April 18 to 20, 2000, NASDA/NASA/CSA conducted a series of real-time HTV capturing operation tests with expanded SSRMS conditions, evaluators, and facility by following schedule.
    Date: Nov. 8th to Nov. 10th, 2000
    Place: Canadian Space Agency Headquarter in Saint-Hubert, Quebec, CANADA
    In this series of tests, Astronaut Doi and other four astronauts executed total of up to 120 simulation- run cases with MOTS (MSS Operations and Training Simulator) in CSA, the facility with more complicated and numerous equipments. Just like previous tests, Astronauts evaluated the operability, by controlling SSRMS and executing capturing operation with free drifting HTV within predefined time. Though the results are still under investigation, the operation time was improved by re-designed operation sequence based on the experience in last tests.
    Photo (Upper): Astronaut Doi trying to capture Photo (Lower): CSA members supporting

    Nov. 9, 2000 Updated

    When crew enters HTV pressurized carrier berthed to ISS, it is necessary to circulate atmosphere in pressured cabin. The fan system for air circulation should meet several requirements such as large flow rate, low noise, lightweight, compact size, and high durability for severe environment during launch. Because each HTV mission period is relatively short, NASDA plans to develop a new air circulation fan system that is appropriate to HTV requirements.
    NASDA is conducting a series of development tests with this new fan system in Shinko-Denki Co. The purpose of tests is to ensure the silent and low vibration design with multi-stage/coaxial concept and new blade/housing shape. NASDA will then review the test results and reflect them to the final fan design.

    Photo: Test Setup

    Oct. 6, 2000 Updated

    The Pre-Shipping Review (PSR) for 28 R-1E thrusters, that will be used for HTV attitude control was held by Primex Space Systems Co. in the United States. These thrusters will be delivered to Ishikawajima-Harima Heavy Industries Co. Then after used in System Firing Test (SFT) in which NASDA confirms the Propulsion-system performance, they will be installed to the first HTV.
    The same thrusters have been used in Space Shuttle for attitude control and they will be installed in Propulsion Module of International Space Station.

    Photo: 28 sets of R-1E thruster (Offered by Primex Space Systems Co.)

    Jul. 7, 2000 Updated

    HTV has two carrier sections, one is a pressurized section which carries the logistics to ISS pressurized section and another is an un-pressurized section which carries experiment devices in ISS exposed section. The exposed experiment devices will be taken out from un-pressurized section with exposed pallet by ISS manipulator (SSRMS).
    From April 10 to June 8, NASDA had conducted Breadboard test in Mizuho facility of Ishikawajima-Harima Heavy Industries Ltd. for Paraffin Actuator that will be used for separation mechanism between exposed pallet and experiment devices. The Paraffin Actuator drives the output pin using phenomena of increasing of volume when paraffin changes its phases from solid to liquid and this attracts attention as a shock-less separation mechanism. In this series of tests, NASDA conducted a nominal driving test, environmental (vacuum/high temperature/low temperature) driving tests and a data-gathering test. NASDA obtained several data and the results will be used to improve the design of HCAM (HTV Cargo Attachment Mechanism).

    May 26, 2000 Updated

    HTV will perform autonomous rendezvous flight to the ISS, however, in the final operation, HTV will be captured by ISS manipulator system (SSRMS) controlled by ISS crew and be berthed to the ISS. Such operation is a peculiar requirement for HTV and we must confirm that it can be certainly captured by ISS crew within the limited time.
    To investigate the feasibility of this operation, a series of SSRMS capturing simulation test was conducted at MD-R (MacDonald Dettwiler Space and Advanced Robotics Limited) in Brampton City, Ontario, Canada from April 18 through 20. Besides four astronauts including Mr. Takao Doi, engineers from NASDA, CSA, and NASA had joined this test.
    In this simulation test, astronauts evaluated by controlling SSRMS and executing capturing operation in computer simulator: MDSF-RT (Manipulator Development and Simulation Facility in Real-Time) which HTV dynamics data from NASDA had been already input. Though details of the result are still under investigation, astronauts judged that this operation is feasible difficulty and it seemed that there are not any critical issues.

    Photo: HTV Capture Real-Time Crew Evaluation (offered by MD-R)

    Apr. 21, 2000 Updated

    In this month, NASA held the following safety review panel toconfirm the HTV safeness regarding to the International Space Station.
    HTV Safety Review Panel (Phase 1): March 13th to March 17th at Johnson Space Center in Houston.
    NASA holds the Safety Review Panel to all segments that compose the ISS and all approaching vehicles in rendezvousing to the ISS. Especially, HTV, which is the first newly designed transfer vehicle, turned out to be reviewed first in this panel. In this review panel, NASA and NASDA members had an animated discussion focused not only upon the hardware safety for the transfer vehicles such as logistics carrier and propulsion system but also upon the safety of flight-plan for rendezvous to the ISS. As a result, NASA confirmed the feasible of the HTV safety design and approved NASDA to progress the next design phase.

    Photo: Safety Review Panel Members

    Jan. 31, 2000 Updated

    PDR (Preliminary Design Review) for SIGI (Space Integrated GPSR/IMU) which is most important sensor of HTV Guidance and Navigation System was conducted at Honeywell co. in Tampa, Florida in United States from Dec. 9 to 10.
    In addition to accelerometers and ring laser gyros for control of HTV attitude/maneuver, this sensor unifies GPS receiver for navigation into one package.
    SIGI is also used in International Space Station to measure the attitude, and H764, the base of SIGI, are used in many aircraft.

    Figure: HTV Guidance and Control Schematic

    Dec. 17, 1999 Updated

    PDR (Preliminary Design Review) for Rendezvous Sensor which to be used during the HTV final approach was conducted at Daimler Chrysler Jena-Optronik in Jena, Germany from Nov.15 to 18. This sensor will also be used for ATV(Autonomous Transfer Vehicle) being developed by ESA.
    We expect a cost reduction / risk decrease become possible by this joint supply of NASDA-ESA.

    The figure: rendezous sensor function during final approach

    Nov. 19, 1999 Updated

    NASDA conducted the Approach/Release (Rendezvous) Flight Technology Test on the ETS-VII, which has close relation to the HTV rendezvous technology from Oct. 26 to 27.
    During the test, ETS-VII tried the R-bar approach which simulates the HTV final approach trajectory to the ISS. HIKOBOSHI satellite regarded as HTV, approached to the virtual R-bar formed by ORIHIME, using the algorithm developed for HTV. As a result, HIKOBOSHI raised the appropriate orbit within the expected corridor determined for rendezvous sensor and successfully finished at the 114 meters close.
    We are now analyzing the data obtained from this experiment. It will greatly contribute to the establishment of all HTV flight algorithm.

    Sep. 17, 1999 Updated

    NASDA held two major review meetings. One was the HTV Phase 1 Safety Review, which examined the HTV design from the point of safety. The another was HTV Preliminary Design Review (PDR), which examined the HTV design from the point of technique.
    The safety review meeting was held from August 18 to 20. The safety design of HTV was generally confirmed. After some additional study, HTV project will take a NASA safety review.
    The HTV PDR meeting was held by NASDA from August 23 to September 3. Approximately forty NASA, European Space Agency (ESA), and Canadian Space Agency (CSA) people attended the meeting and examined the HTV design. As the result of review, design of HTV was confirmed to be adequate. Therefore, the production of HTV Engineering Model (EM) and the progress to detailed design phase were admitted.

    Jul. 26, 1999 Updated

    The documents for PDR (Preliminary Design Review), which will be conducted from July 15th to September 3rd have been released. These documents have also been sent to NASA, CSA, and ESA in the end of June.
    We will continue to coordinate with reviewers of both NASDA and other organizations on matters which they point out until PDR Main Board.
    At the same time, the documents for Phase 1 Safety Review have been released.

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  • [Project Topics] KOUNOTORI5 launch rescheduled to 8:50:49 p.m. on August 19 (Wed.) 2015

    Topics List

    Aug. 17, 2015 Updated
    KOUNOTORI5 launch rescheduled to 8:50:49 p.m. on August 19 (Wed.) 2015

    The KOUNOTORI5(HTV5)/H-IIB F5 launch was postponed to 8:50:49 p.m. on August 19 due to adverse weather.
    Accordingly, the live launch report will begin at 8:00 p.m. on August 19 (Wed. , JST). The report will be broadcast through the Internet.
    Please send your support messages for the mission, or tweet it including the hashtag #HTV5.

    KOUNOTORI5 launch rescheduled to 8:50:49 p.m. on August 19 (Wed.) 2015

    Aug. 16, 2015 Updated
    KOUNOTORI5 launch postponed to Aug. 19 (Wed., JST)

    The launch date of the H-IIB Launch Vehicle No. 5 carrying the KOUNOTORI5 has been postponed as unfavorable weather is forecasted. The launch was originally scheduled for August 17. The live broadcast of the launch will also be put off accordingly.
    Your support messages are very much welcome through Twitter (Hashtag “#HTV5”) or via the following website.

    KOUNOTORI5 launch postponed to Aug. 19 (Wed., JST)

    Aug. 15, 2015 Updated
    New launch date and time of KOUNOTORI5/H-IIB F5 decided

    Aug. 14, 2015 Updated
    KOUNOTORI5 launch postponed to Aug. 17 (Mon., JST)

    The launch date of the H-IIB Launch Vehicle No. 5 carrying the KOUNOTORI5 has been postponed as unfavorable weather is forecasted. The launch was originally scheduled for August 16. The live broadcast of the launch will also be put off accordingly.
    Your support messages are very much welcome through Twitter (Hashtag “#HTV5”) or via the following website.

    KOUNOTORI5 launch postponed to Aug. 17 (Mon., JST)

    Jul. 21, 2015 Updated
    Dates set for capturing the KOUNOTORI5 and its berthing with ISS Astronaut Yui to be in charge of operation

    After international coordination, the dates for capturing the KOUNOTORI5, a cargo transporter to the International Space Station (ISS), and its berthing have been respectively set as August 20 (Thu.) and 21 (Fri.) The KOUNOTORI5 is scheduled to be launched on August 16 (Sun.) from the Tahegashima Space Center.
    It was also decided that Astronaut Kimiya Yui will manipulate the ISS robotic arm to capture the KOUNOTORI2.

    Dates set for capturing the KOUNOTORI5 and its berthing with ISS Astronaut Yui to be in charge of operation

    Jul. 10, 2015 Updated
    KOUNOTORI5 and operation simulation training opened to the press

    On July 1, the KOUNOTORI5, a cargo transporter to the ISS, was revealed to the media at the Tanegashima Space Center. The mission was also explained there.
    From the evening of July 9 to the morning of the 10th, simulation training for the KOUNOTORI5 operation and control was held in the KOUNOTORI operation room at the Tsukuba Space Center, and part of it was also open to the press. This training was a last opportunity for a joint session between JAXA and NASA before the KOUNOTORI5 launch. On the NASA side, Astronaut Wakata participated in the training as a CAPCOM (capsule/spacecraft communicator).

    KOUNOTORI5 and operation simulation training opened to the press

    Jun. 9, 2015 Updated
    Launch day set for KOUNOTORI5/H-IIB F5!

    The launch date and time for the H-IIB Launch Vehicle No. 5 (H-IIB F5) with the H-II Transfer Vehicle “KOUNOTORI5” (HTV5) onboard was set for around 10:01 p.m. on August 16 (Sun.), 2015 (Japan Standard Time).
    The H-IIB F5 has already been transported to the TNSC, and it is now being assembled there.
    * Launch time will be determined by the updated orbit of the ISS.

    Launch day set for KOUNOTORI5/H-IIB F5!

    Sep. 7, 2013 Updated
    KOUNOTORI4 completed its mission with re-entry!

    The KOUNOTORI4 (HTV4, a cargo transporter to the International Space Station) left the ISS on Sept. 5 and re-entered the atmosphere at 3:37 p.m. on Sept. 7 (Japan Standard Time.)
    The KOUNOTORI 4 successfully achieved its mission of taking cargo to the ISS, then completed all its tasks over about 36 days.
    We would like to send our sincere appreciation to all of you who have been supporting the KOUNOTORI project.

    KOUNOTORI4 completed its mission with re-entry!

    Sep. 3, 2013 Updated
    Re-entry date and time for KOUNOTORI4 decided

    Schedules of departure from the International Space Station (ISS) and of re-entry to the atmosphere for the H-II Transfer Vehicle “KOUNOTORI 4” (HTV4) are determined as follows.

    Departure from the ISS:
    September 5, 2013 / 1:00 a.m.(Japanese Standard Time, JST)*
    Re-entry to the atmosphere:
    September 7, 2013 / 3:36 p.m.(JST)*

    * The time may vary according to the actual operation.

    Aug. 10, 2013 Updated
    KOUNOTORI4 berthed at ISS!

    The KOUNOTORI4 (HTV4, a cargo transporter to the International Space Station) was captured by the ISS robotic arm at 8:22 p.m. on August 9 (Japan Standard Time) and berthed at the ISS at 3:38 a.m. on August 10 (JST). The KOUNOTORI4 was launched by the H-IIB Launch Vehicle No.4 on August 4. ISS astronauts will take cargo out from the Pressurized and Unpressurized Logistic Carriers into the ISS.

    Aug. 9, 2013 Updated
    Live broadcast of KOUNOTORI4 trip to ISS!

    The KOUNOTORI3 (HTV4, the cargo transporter to the International Space Station) launched on August 4 has been traveling to the ISS while adjusting its altitude. Between the evening on August 9 and early on the morning of August 10, the KOUNOTORI4 will make a final approach and berth at the ISS. JAXA will provide a live broadcast of its final access, capture, and berthing.
    The KOUNOTORI4’s approach and the ISS’s capture of the vehicle by the robotic arm is scheduled for about one hour from 7:40 p.m. on the 9th (Japan Standard Time.) Then the telecast of its berthing will last for about one hour from 22:00 p.m. on the 9th (JST.)
    Please don’t miss the broadcast!
    (Photo: The KOUNOTORI3 approaching the ISS, JAXA/NASA)

    Aug. 4, 2013 Updated
    Launch Success of KOUNOTORI4/H-IIB F4

    The H-IIB Launch Vehicle No. 4 with the KOUNOTORI4 (HTV4, a cargo transporter to the International Space Station) onboard lifted off from the Tanegashima Space Center at4:48:46 a.m. on August 4 (Sun., Japan Standard Time.)
    The launch vehicle flew smoothly, and at 14 minutes and 59 seconds after liftoff, the KOUNOTORI4 separation was confirmed.
    The KOUNOTORI4 will gradually go closer to the International Space Station, and it will be berthed at the ISS. We will broadcast the berthing on our website, so don’t miss it!

    Jun. 19, 2013 Updated
    KOUNOTORI4 revealed at TNSC

    On June 19, the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) “KOUNOTORI4” was shown to the media at the Tanegashima Space Center (TNSC.)
    The KOUNOTORI4 will be launched by the H-IIB Launch Vehicle No. 4 on Aug. 4 from the TNSC. It will carry various goods to the ISS including food and water for astronauts, as well as experiment devices and materials for the Japanese Experiment Module “Kibo.” Launch preparations continue for the KOUNOTORI4.

    May 21, 2013 Updated
    KOUNOTORI4/H-IIB F4 launch schedule decided!

    The H-IIB Launch Vehicle No. 4 (H-IIB F4) carrying the H-II Transfer Vehicle (HTV4, a cargo transporter to the International Space Station) will be launched on August 4 (Sunday, Japan Standard Time.) The launch time will be around 4:48 a.m. (JST.) It will be blasted off from the Yoshinobu Launch Complex at the Tanegahsima Space Center. Why don’t you take this opportunity to come to Tanegahima to witness the liftoff at hand!

    Sep. 14, 2012 Updated
    KOUNOTORI3 completed its mission with re-entry!

    The KOUNOTORI3 (HTV3, a cargo transporter to the International Space Station) left the ISS on Sept. 13 and re-entered the atmosphere at 2:27 p.m. on Sept. 14 (Japan Standard Time.)
    The KOUNOTORI 3 successfully achieved its mission of taking cargo to the ISS, then completed all its tasks over about 56 days.
    We would like to send our sincere appreciation to all of you who have been supporting the KOUNOTORI project.

    Sep. 11, 2012 Updated
    KOUNOTORI3 departure and re-entry live report!

    The H-II Transfer Vehicle “KOUNOTORI3” (HTV3,a cargo transporter to the International Space Station) will leave from the ISS at around 0:50 a.m. on Sept. 13 (Japan Standard Time, all the following dates and time are JST,) and will re-enter the atmosphere at around 2:24 p.m. on Sept. 14.
    JAXA will offer a live report of its departure from the ISS from 0:20 a.m. on the 13th (Thu.), then a live scene of the HTV operation room at the time of its re-entry from 1:45 p.m. on the 14th (Fri.) through the Internet. Please do not miss the footage!

    Sep. 7, 2012 Updated
    Re-entry date and time for KOUNOTORI3 decided

    The re-entry schedule for the KOUNOTORI3 was set as follows after extended mooring at the International Space Station due to an additional extravascular activity.

    Departure from the ISS:
    September 13, 2012 / 0:50 a.m.(Japanese Standard Time, JST)*
    Re-entry to the atmosphere:
    September 14, 2012 / 2:24 p.m.(JST)*

    * The time is subject to change due to actual operational status.

    The KOUNOTORI3 will carry a re-entry data recorder, the i-Ball, which was developed in cooperation between the public and private sectors to acquire atmosphere re-entry data as well as scenes of KOUNOTORI3’s destruction.

    Jul. 28, 2012 Updated
    KOUNOTORI3 berthed at ISS!

    The KOUNOTORI3 (HTV3, a cargo transporter to the International Space Station) was captured by the ISS robotic arm at 9:23 p.m. on July 27 (Japan Standard Time) and berthed at the ISS at 2:31 a.m. on July 28. The KOUNOTORI3 was launched by the H-IIB Launch Vehicle No.3 on July 21. ISS astronauts will take cargo out from the Pressurized and Unpressurized Logistic Carriers into the ISS.
    (Photo: The KOUNOTORI3 to a Common Berthing Mechanism at the nadir port of Harmony, JAXA/NASA)

    Jul. 21, 2012 Updated
    Launch Success of KOUNOTORI3/H-IIB F3

    The H-IIB Launch Vehicle No. 3 with the KOUNOTORI3 (HTV3, a cargo transporter to the International Space Station) onboard lifted off from the Tanegashima Space Center at 11:06:18 on July 21 (Sat., Japan Standard Time.)
    The launch vehicle flew smoothly, and at 14 minutes and 53 seconds after liftoff, the KOUNOTORI3 separation was confirmed.
    The KOUNOTORI3 will gradually go closer to the International Space Station, and it will be berthed at the ISS. We will broadcast the berthing on our website, so don’t miss it!

    Jun. 21, 2012 Updated
    KOUNOTORI3/H-IIB F3 Special Site now open!

    JAXA will launch the KOUNOTORI3 (a cargo transporter to the International Space Station, ISS) by H-IIB Launch vehicle No.3 on July 21 from the Tanegashima Space Center. We have opened the KOUNOTORI3/H-IIB F3 Special Site to be ready for the launch.
    Please check the special site for more information. We have also started welcoming your support messages, so please send them to us!

    Jun. 7, 2012 Updated
    KOUNOTORI3 revealed to the media at TNSC

    On June 1 (Fri.), the H-II Transfer Vehicle “KOUNOTORI3” (HTV3, a cargo transporter to the International Space Station) was revealed to the media at the Spacecraft and Fairing Assembly Building 2 at the Tanegashima Space Center. The KOUNOTORI3 will be packed with food and daily necessities for astronauts aboard the ISS, test equipment for aquatic organisms, and other experiment devices including a small satellite, then will be launched by the H-IIB Launch Vehicle No. 3 at 11:18 a.m. on July 21, 2012 (Japan Standard Time.) The KOUNOTORI is currently under preparations for its journey to space.

    Mar. 21, 2012 Updated
    KOUNOTORI3/H-IIB F3 launch schedule decided!

    The launch date and time for the H-IIB Launch Vehicle No. 3 (H-IIB F3) with the H-II Transfer Vehicle “KOUNOTORI3” (HTV3), a cargo transporter to the International Space Station, has been set to be at around 11:18 a.m. on July 21 (Sat.), 2012 (Japan Standard Time.) The launch preparation operation for the KOUNOTORI is smoothly in progress at the Tanegashima Space Center.

    Mar. 30, 2011 Updated
    KOUNOTORI2 re-entered the atmosphere to complete its mission!

    The KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station,) which left the ISS at around 0:46 a.m. on March 29 (Japan Standard Time,) re-entered the atmosphere at around 12:09 p.m. on March 30 (JST.)
    The KOUNOTORI2 successfully completed its role to transport materials to the ISS, then re-entered the Earth’s atmosphere to complete its mission of approximately 67 days.
    Thank you very much for supporting the KOUNOTORI2 and H-IIB Launch Vehicle No.2 missions.

    Mar. 29, 2011 Updated
    KOUNOTORI2 left ISS!

    The KOUNOTORI2 (HTV2, a cargo transporter to the ISS) was detached from the International Space Station (ISS) using the ISS robotic arm at 10:29 p.m. on March 28 (Japan Standard time,) and it emitted a jet to leave the ISS after being transported to the release point at 0:46 a.m. on the 30th.
    The KOUNOTORI2 will re-enter the Earth’s atmosphere at around 12:09 on March 30. From some areas, you can see the KOUNOTORI2 flying around the Earth between the 29th and the 30th. Also, please witness the scene of the HTV operation and control room when it re-enters the atmosphere through the live Internet broadcast, which will begin at 11:30 a.m. on the 30th.

    Mar. 25, 2011 Updated
    KOUNOTORI2 leaving ISS on the 29th! Live broadcast scheduled

    The KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station) will depart from the ISS with used material loaded on March 29 (Japan Standard Time,) and will be slated for re-entry to the atmosphere on the 30th (JST.) JAXA will broadcast a live Internet report of the KOUNOTORI departure from the ISS from 0:00 a.m. on the 29th (JST,) then its re-entry to the atmosphere from 11:30 a.m. on the 30th (JST.) Please watch the events through the Internet!

    Mar. 22, 2011 Updated
    KOUNOTORI2 to leave ISS

    The departure date of the KOUNOTORI2 (HTV2, a cargo transporter to the ISS), which is loaded with used materials, from the International Space Station (ISS) has been decided.
    The KOUNOTORI2 will leave the ISS at around 0:45 a.m. on March 29 (Japan Standard Time) after completing its role at the ISS. After departure, it will be burned when it re-enters the atmosphere at around 12:10 p.m. on March 30. Following its combustion, its mission will be accomplished.
    We will broadcast a live report of the departure and re-entry of the KOUNOTORI2. More details will be posted on our website. (Photo by NASA)

    Mar. 11, 2011 Updated
    KOUNOTORI2 relocation to the earth-facing port completed

    At 8:49 p.m. on March 10 (Japan Standard Time), the KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station) began to be moved from the zenith port to the earth-facing port using the robotic arm of the International Space Station. At 3:55 a.m. on the 11th (JST,) KOUNOTORI2’s electric and communication systems were connected to the ISS to complete the relocation. After being loaded with used items, the KOUNOTORI2 will re-enter the atmosphere to be burned.

    Mar. 9, 2011 Updated
    KOUNOTORI2 to return to earth-facing port from March 10

    The KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station), will move back to the earth-facing port of the Harmony (Node 2) from its zenith port now that the Space Shuttle Discovery left the ISS to go home on March 7 (Japan Standard Time.) The relocation is scheduled to be performed on the 10th and 11th (JST.) More cargo will be taken out of the KOUNOTORI2, then, after being packed with used materials, the KOUNOTORI2 will re-enter the atmosphere.
    (Photo by NASA)

    Feb. 21, 2011 Updated
    KOUNOTORI2 relocation to the zenith port completed

    As part of preparations for the Space Shuttle Discovery’ s docking with the International Space Station (ISS,) the KOUNOTORI2 , or the HTV2, a cargo transporter to the ISS, was moved from the earth-facing port of the Harmony (Node 2) to its zenith port. This was the first time to perform such a relocation. The KOUNOTORI2 was successfully transported at 1:45 a.m. on Feb. 19 (Japan Standard Time,) and the electric cables were connected with the Harmony at 4:26 a.m. (JST) to complete its relocation.

    Jan. 28, 2011 Updated
    KOUNOTORI2 berthing at ISS

    The KOUNOTORI2, or the HTV2, a cargo transporter to the International Space Station (ISS) launched by the H-IIB Launch Vehicle No.2, was captured by the ISS robotic arm at around 8:41 p.m. on January 27 (Japan Standard Time,) and, at around 3:34 a.m. on the 28th (JST,) the KOUNOTORI berthed at the ISS. Cargo in the Pressurized Section will be transported to the ISS by the ISS astronauts followed by cargo in unpressurized areas.

    Jan. 22, 2011 Updated
    KOUNOTORI2/H-IIB F2 successfully launched

    The H-IIB Launch Vehicle No. 2 with the KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station, ISS) onboard was launched from the Tanegashima Space Center at 2:37:57 p.m. on January 22 (Sat., Japan Standard Time.) The launch vehicle flew smoothly, and, at about 15 minutes and 13 seconds after liftoff, the separation of the KOUNOTORI2 was confirmed.
    The KOUNOTORI2 will fly to the ISS, then, on Jan. 28 (Fri., JST,) it is slated for berthing with the ISS.

    Dec. 14, 2010 Updated
    KOUNOTORI2 system checkup completed

    At the Tanegashima Space Center, all parts of the H-II Transfer Vehicle “KOUNOTORI2” (HTV2) were integrated electrically and mechanically in the end of October. Throughout November, the assembled KOUNOTORI2 has been checked as one system to confirm that no problem was found in the vehicle.
    After a thorough inspection, propellants were loaded onto the KOUNOTORI2 tanks, and currently the tank pressure is being adjusted. Preparation for launch is smoothly progressing.
    The final launch preparation including battery charge and loading onto the H-IIA Launch Vehicle No.2 will now be carried out for the KOUNOTORI2.

    Dec. 1, 2010 Updated
    KOUNOTORI2 control and operation simulation revealed to the press

    On November 30, JAXA showed part of the control and operation simulation of the KOUNOTORI2 to the media at the Tsukuba Space Center. The KOUNOTORI2 (HTV2) is a cargo transfer vehicle to the International Space Station (ISS.)
    The purpose of the simulation was to train and improve operators’ skills. It takes about 20 hours with NASA to simulate events, from the KOUNOTORI2’s arrival at around 12-km beneath the ISS, to its gradual approach to the ISS, to the capture of the KOUNOTORI2 by the ISS robotic arm, and then the docking of the KOUNOTORI2.

    Nov. 26, 2010 Updated
    KOUNOTORI2 shown to the Press at TNSC

    On Nov. 25, the H-II Transfer Vehicle “KOUNOTORI”2 (a cargo transporter to the International Space Station) was revealed to the media at the Spacecraft and Fairing Assembly Building No. 2 at the Tanegashima Space Center. We are engaging in preparation for the launch of the KOUNOTORI2 including propellant loading and mating with the launch vehicle.
    JAXA provides updated information about the KOUNOTORI2 and H-IIB Launch Vehicle No.2 at the special site. Your support messages are welcome there, too.

    Nov. 11, 2010 Updated
    HTV nickname selected & special site open!

    “KOUNOTORI” (meaning “a white stork” in English) was chosen as the nickname of the H-II Transfer Vehicle (HTV, a cargo transfer vehicle to the International Space Station.)
    During a month-long nickname campaign, we received 17,236 suggestions.
    Among them, “KOUNOTORI” was selected because a white stork carries an image of conveying an important thing (a baby, happiness, and other joyful things); therefore, it precisely expresses the mission to transport essential materials to the ISS.
    The KOUNOTORI2 is scheduled to be launched by the H-IIB Launch Vehicle No. 2 (H-IIB F2) at around 3:29 p.m. (Japan Standard Time) on January 20 (Thu.), 2011.
    Taking this opportunity of selecting the nickname, we would also like to open the “KOUNOTORI2/H-IIB F2 Special Site.” We will provide you with updated information about the project including a column by project personnel and launch related matters. Please enjoy the site!
    * Launch time will be determined by the updated orbit of the ISS.

    Nov. 10, 2010 Updated
    Launch day set for HTV2/H-IIB F2!

    The launch date and time for the H-IIB Launch Vehicle No. 2 (H-IIB F2) with the H-II Transfer Vehicle (HTV2) onboard was set for around 3:29 p.m. on January 20 (Thu.), 2011 (Japan Standard Time). The HTV2 is a cargo transporter to the International Space Station (ISS.) The integration of all modules of the HTV2 was completed at the Tanegashima Space Center (TNSC), and it will enter the final launch preparation phase. The H-IIB F2 has already been transported to the TNSC, and it is now being assembled there.
    * Launch time will be determined by the updated orbit of the ISS.

    Nov. 2, 2010 Updated
    HTV2: all modules connected, moved to final launch preparations

    (Left) All HTV2 modules are being connected (Center) Integrated HTV2 (front side) (Right) Integrated HTV2 (back side) (Images by JAXA)

    On Oct. 29, we completed connecting all modules of the second H-II Transfer Vehicle (HTV2, a cargo transporter to the International Space Station) electrically and mechanically at the Second Spacecraft and Fairing Assembly Building (SFA2) at the Tanegashima Space Center. The HTV2 is now in its configuration for launch.
    After a comprehensive check on the integrated HTV2, it will go through final launch preparations including propellant loading and fairing encapsulation. The HTV2 is scheduled to be launched in the winter launch period of Japan Fiscal Year 2010.

    Oct. 13, 2010 Updated
    Full assembly started for the second HTV

    The assembly operation for all modules of the second H-II Transfer Vehicle (HTV, the cargo transporter to the International Space Station) started on October 6 at the second Spacecraft and Fairing Assembly Building (SFA2) at the Tanegashima Space Center. Prior to full assembly, in mid September, cargo to the ISS was loaded onto the Pressurized and Unpressurized Carriers.

    Apr. 7, 2010 Updated
    Development of HTV/H-IIB received Japan industry technology/MEXT award

    JAXA was selected as one of 12 organizations to receive the Ministry of Education, Culture, Sports, Science and Technology award at the 39th Japan industry technology awards for its development of the HTV and H-IIB launch vehicle.
    The Japan industry technology awards are presented by Nikkan Kogyo Shimbun Ltd. (Business and Technology Daily News, Japan) to encourage development of original and unique technology that contributes to the promotion of industry. The news company bestows the awards to development projects of distinctive large-scale technological systems.

    Feb. 10, 2010 Updated
    HTV Project Team awarded for research

    Since 2005, the National Institute of Science Technology Policy (NISTEP) of the Ministry of Education, Culture, Sports, Science and Technology (MEXT) has been choosing researchers who have made significant contributions to science and technology every year to praise their efforts. In 2009, the demonstration flight of the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) was highly evaluated, and on February 9, Mr. Torano, HTV Project Manager, Mr. Koyari, Sub-project Manager, and Mr. Sasaki, Functional Manager, received a memento of the selection.

    Nov. 2, 2009 Updated
    HTV re-entered the atmosphere, mission completed

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which departed from the International Space Station (ISS) on October 31, re-entered the atmosphere at around 6:26 a.m. on November 2.
    The HTV successfully completed its cargo transportation operations to the ISS, and accomplished all its missions in about 52 days following the re-entry today.

    Oct. 31, 2009 Updated
    HTV released from ISS

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which completed its cargo transportation mission at the International Space Station (ISS), was unberthed from the ISS by its robotic arm (SSRMS) at 0:02 a.m. on October 31 (Japan Standard Time, the following dates and times are JST.) The HTV departed from the ISS at 2:32 a.m. on the 31st. The HTV will leave the ISS orbit, and is scheduled to re-enter the Earth’s atmosphere at around 6:25 a.m. on November 2 (Mon.)
    You may be able to see the HTV just prior to re-entry from Okinawa at around 6:13 a.m. on the 2nd if the deorbit process goes smoothly and the weather cooperates. (Photo by NASA)

    Oct. 27, 2009 Updated
    Internet Live Report: HTV leaving ISS on Oct. 31 (Sat)

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which is currently berthed at the International Space Station (ISS), is scheduled to depart from the ISS at 2:30 a.m. on Oct. 31 (Sat) (Japan Standard Time, all the following days and times are in JST.) The HTV will be unberthed from the ISS by the ISS robotic arm (SSRMS) late at night on Oct. 30 (Fri) after its hatch to the ISS is closed at dawn of Oct. 30, then depart from the ISS. If everything goes smoothly, the HTV will re-enter the Earth’s atmosphere around 6:25 a.m. on Nov. 2 (Mon).

    We will broadcast a live report of the HTV unberthing and departure from the ISS through the Internet from 11:45 p.m. on Oct. 30 (Fri) and from 2:15 a.m. on Oct. 31 (Sat) respectively. (Sorry, the live reports are broadcasted only in the Japanese language.) Please enjoy the HTV live reports over the weekend!
    The live broadcast time schedule has changed due to the delay of the HTV departure.

    Oct. 21, 2009 Updated
    The HTV PLC unloading operations completed, trash loading continues

    HTV-1, being berthed to the ISS, is operating nominally. The Small Fine Arm (SFA) of the Kibo Remote Manipulator System (JEMRMS), packed in a Cargo Transfer Bag (CTB) and delivered to the ISS, was transferred from the HTV Pressurized Logistics Carrier (PLC) to Kibo on October 4. The Pressurized Stowage Resupply Rack (PSRR), also delivered on the HTV-1, was transferred to Kibo’s Experiment Logistics Module-Pressurized Section (ELM-PS) on October 14. All the cargo transfer operation from the HTV PLC to the ISS was completed on October 20.
    Aboard the ISS, trash loading into the HTV PLC is currently underway. With this trash stow activity completed, the HTV-1 will depart from the ISS, and enter the atmosphere early next month.
    Photo (provided by NASA): Astronaut Robert Thirsk taking cargo out from the HTV Pressurized Carrier.

    Oct. 14, 2009 Updated
    HTV operations running smoothly, cargo unloading continues

    Cargo unloading operations continued from the Pressurized Logistics Carrier of the H-II Transfer Vehicle (HTV) Demonstration Flight berthed at the International Space Station (ISS). On Oct. 4, the Small Fine Arm (SFA) of the Kibo’s Robotic Arm was moved to the ISS. The SFA was transported to the ISS as it was still packed in the Cargo Transfer Bag. One unit of the Pressurized Stowage Resupply Rack will be transferred to the ISS on the 14th.
    Photo (provided by NASA): Astronaut Nicole Stott taking cargo out from the HTV Pressurized Carrier.

    Sep. 26, 2009 Updated
    Exposed Pallet stored back in HTV

    The Exposed Pallet of the H-II Transfer Vehicle (HTV) Demonstration Flight was retrieved and stored back in the HTV Unpressurized Carrier at 10:20 p.m. on Sept. 25 (Japan Standard Time) by the robotic arms of the Kibo and the International Space Station (SSRMS) after its two cargoes, the experiment devices in the unpressurized environment, had been installed in the Kibo’s Exposed Facility.
    Cargo in the HTV Pressurized Carrier will now be unloaded by the astronauts aboard the ISS. After the unloading, used material and equipment on the ISS will be packed into the Pressurized Carrier. The HTV will depart from the ISS in mid-November to re-enter the atmosphere. (The detailed schedule will be decided based on the ISS/HTV operational status.) (Photo by NASA)

    Sep. 25, 2009 Updated
    Two experiment devices installed onto Kibo Exposed Facility

    On Sept. 24 and 25 (Japan Standard Time), two experiment devices that were shipped by the H-II Transfer Vehicle (HTV) Demonstration Flight were unloaded from the HTV Exposed Pallet and installed onto the Exposed Facility of the Japanese Experiment Module “Kibo.”
    The two devices are the “Superconducting Submilimeter-Wave Limb-Emission Sounder (SMILES)” and the “Hyperspectral Imager for the Coastal Ocean (HICO) & Remote Atmospheric & Ionospheric Detection System (RAIDS) Experimental Payload (HREP.)” The HREP and the SMILES were mounted at 8:15 p.m. on the 24th and 1:12 a.m on the 25th respectively. (Photo by NASA)

    Sep. 24, 2009 Updated
    HTV Exposed Pallet attached to the Kibo Exposed Facility

    At 6:06 p.m. on Sept. 23rd (Japan Standard Time, JST), the Exposed Pallet was taken out from the H-II Transfer Vehicle (HTV) Demonstration Flight, which is now berthed at the International Space Station (ISS). The Pallet was then attached onto the Exposed Facility of the Japanese Experiment Module “Kibo” at 11:33 p.m. (JST). The experiment devices on the Pallet will be moved to be installed onto the Kibo’s Exposed Facility. (Photo by NASA)

    Sep. 18, 2009 Updated
    HTV Demonstration Flight successfully berthed at ISS

    The H-II Transfer Vehicle (HTV) Demonstration Flight, launched by the H-IIB Launch Vehicle Test Flight at 2:01 a.m. on Sept. 11 (Japan Standard Time, JST,) took almost one week to approach the International Space Station (ISS) and arrived at the Berthing Point 10 meters below the ISS at 4:27 a.m. on the 18th (JST, following times are all JST.) At 4:51 a.m., the HTV was captured by the ISS robotic arm (Space Station Remote Manipulator System, SSRMS) manipulated by the ISS crew, and it was installed onto the Common Berthing Mechanism (CBM) on the lower side (earth side) of the Harmony (Node 2) at 7:26 a.m. At 10:49 a.m., electric and communication lines were connected, and the HTV was successfully berthed at the ISS.

    Sep. 15, 2009 Updated
    Live reports of the HTV final approach to the ISS on Sept. 18 (Fri.)

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which was launched by the H-IIB Launch Vehicle at 2:01:46 a.m. on September 11 (Fri.) has been smoothly flying on its scheduled course. Its final approach to the International Space Station (ISS) was approved at the ISS Mission Management Team (IMMT) meeting on Sept. 15, thus, from the 16th, the altitude of the HTV will be maneuvered to gradually approach the ISS. The HTV is scheduled to be berthed at the ISS on Sept. 18 (Fri.)
    JAXA will broadcast the live reports of the ISS robotic arm capturing the HTV from 4:00 a.m., and the berthing of the HTV at the ISS from 7:00 a.m. They are early in the morning, but don’t miss them!

    Sep. 11, 2009 Updated
    HTV/H-IIB Successfully Launched!!

    The Japan Aerospace Exploration Agency (JAXA) launched the H-II Transfer Vehicle (HTV) Demonstration Flight aboard the H-IIB Launch Vehicle Test Flight (H-IIB TF1) at 2:01:46 a.m. on September 11, 2009 (Japan Standard Time, JST) from the Tanegashima Space Center. The launch vehicle flew smoothly, and, at about 15 minutes and 6 seconds after liftoff, the separation of the HTV Demonstration Flight was confirmed.

    The HTV will gradually approach the International Space Station (ISS) and berth at the ISS on the 18th (Friday, JST.)

    Aug. 31, 2009 Updated
    HTV moved to the VAB! Final launch preparation phase

    On August 30, the encapsulated HTV Demonstration Flight was transported to the Vehicle Assembly Building (VAB.) It will be loaded onto the H-IIB Launch Vehicle to be ready for the launch on September 11. We published a promotion movie of the HTV/H-IIB mission. Please watch it before witnessing the actual launch!

    Aug. 24, 2009 Updated
    HTV encapsulated

    On August 21, the H-II Transfer Vehicle (HTV) Demonstration Flight was mated with the Payload Attach Fitting (PAF) at the Spacecraft and Fairing Assembly Building #2.
    On the 23rd, the HTV on the PAF was encapsulated by the payload fairing, which covers the payload to protect it from air resistance, friction and the acoustic vibrations of launch. The fairing for the HTV is a 5S-H type and is about 5 meters in diameter and about 15 meters in length. It was developed for the HTV launch.
    The encapsulated HTV Demonstration Flight will be transported to the Vehicle Assembly Building (VAB) and loaded onto the H-IIB Launch Vehicle Test Flight.

    Jul. 9, 2009 Updated
    HTV opened to the press at TNSC

    On July 9, the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) was opened to the press at the Spacecraft and Fairing Assembly Building #2 (SFA2) at the Tanegashima Space Center (TNSC.)
    We are providing updated information on the HTV and H-IIB at the HTV/H-IIB Special Site.

    Jul. 8, 2009 Updated
    HTV/H-IIB launch date decided! Special site opened

    The H-IIB Launch Vehicle Test Flight with the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) will be launched at 2:04 a.m. on September 11 (Fri.). (*)
    The HTV has been fully assembled at the Tanegashima Space Center, and it will be under final launch preparations including comprehensive checkout and propellant loading to be ready for launch.
    The ground comprehensive test for the H-IIB Launch Vehicle using the Ground Test Vehicle (the GTV test) is scheduled on the 11th.
    Please check the updated information on the HTV and H-IIB at the “HTV/H-IIB Special Site,” which was opened today. We hope you enjoy the site.
    (*) Time will be determined by the updated orbit of the International Space Station (ISS.)

    Jun. 30, 2009 Updated
    Preparations for the HTV Demonstration Flight going smoothly at TNSC

    Preparations for the Demonstration Flight of the H-II Transfer Vehicle (HTV) are underway at the Tanegashima Space Center (TNSC).
    At dawn on April 23, the HTV arrived at the TNSC and was moved into the Spacecraft and Fairing Assembly Building #2 for a post-transportation inspection on each element of the vehicle.
    Payloads to be shipped to the International Space Station (ISS) by the HTV were then loaded onto the HTV’s Pressurized Logistic Carrier and Unpressurized Logistic Carrier.

    In the Pressurized Logistic Carrier, life-related supplies, such as food and clothes, which were packed in the Cargo Transfer Bag (CTB) and other experiment materials were stored on the HTV Re-supply Rack (HRR) of the Carrier. In the Unpressurized Logistic Carrier, the Superconducting Submilimeter-Wave Limb-Emission Sounder (SMILES,) which is an experiment device for the Kibo’s Exposed Facility, and NASA experimental equipment were loaded onto the Exposed Pallet of the Carrier.

    After completing the payload loading, the two carriers were mated.
    On June 24, all HTV modules including the Avionics Module and Propulsion Module were connected.
    The HTV demonstration flight is now fully assembled, and will start final launch preparations such as a comprehensive vehicle inspection and propellant loading.

    Apr. 24, 2009 Updated
    HTV arrives at TNSC

    At dawn on April 23, the First H-II Transfer Vehicle (HTV) was transported from Shimama Port at Tanegashima to the Tanegashima Space Center (TNSC.) The HTV left the Tsukuba Space Center on April 17. The Pressurized Logistic Carrier, Unpressurized Logistic Carrier, the Avionics Module, and the Propulsion Module were detached for the transportation, thus they will be assembled after arrival. A final functional checkup will be held prior to the launch.

    Apr. 17, 2009 Updated
    HTV left for the TNSC

    The first H-II Transfer Vehicle (HTV), or the HTV Technology Demonstrator, left the Tsukuba Space Center at dawn on April 17, 2009, for the Tanegashima Space Center (TNSC.) After arrival, the HTV will be assembled and checked for launch by the H-IIB Launch Vehicle, which is now under testing.


    The first HTV leaving the TKSC (Unpressurized Logistics Carrier, Avionics Module, and Plopulsion Module)

    The first HTV arrived at Tsuchiura Port
    (Unpressurized Logistics Carrier)

    Dec. 26, 2008 Updated
    HTV open to the press

    On Dec. 25, 2008, JAXA revealed the maiden H-II Transfer Vehicle (HTV), an unmanned supply transfer vehicle that will fly to the International Space Station (ISS), to the press at the Tsukuba Space Center (TKSC.) It was the first press conference since assembling all the modules of the first HTV.

    At the press conference, the HTV and its launch by the H-IIB Launch Vehicle were explained by HTV Project Manager Yoshihiko Torano and H-IIB Launch Vehicle Project Manger Tomihisa Nakamura. The Superconducting Submilimeter-Wave Limb-Emission Sounder (SMILES,) which will be transported to the ISS by the first HTV, was also introduced by Professor Masato Shiotani of the Research Institute for Sustainable Humanosphere of Kyoto University. The SMILES is one of the experiment devices that will be installed onto the Exposed Facility of the Japanese Experiment Module “Kibo.”

    Also at the press conference, the first HTV and the SMILES undergoing an all-vehicle functional test were shown to the media at the Spacecraft Integration and Test Building at the TKSC. The modules of the cargo section (“Pressurized Carrier” and “Unpressurized Carrier,”) “Avionics Module” and “Propulsion Module” were assembled for the test. The “Exposed Pallet” loaded with a dummy cargo for the test and the SMILES were also displayed.

    We will conduct comprehensive functional tests with the mechanically and electrically integrated HTV, such as conductivity verification of the pipes and electric system, and other compatibility tests. The HTV is then scheduled to be transported to the Tanegashima Space Center in April, 2009, at the earliest, and be launched by the H-IIB Launch Vehicle in the summer launch season of 2009 or later.

    Dec. 18, 2008 Updated
    All flight modules assembled for first time for inaugural HTV flight

    On Dec. 12, all the parts of the H-II Transfer Vehicle (HTV,) the supply transfer vehicle to the International Space Station, were assembled for an all-vehicle functional test ahead of its first flight. They are the “Logistic Carrier Pressurized Section,” the cargo section of the “Un-pressurized Carrier,” the “Exposed Pallet,” the “Avionics Module” and the “Propellant Module.” This was the first time that all the modules were assembled. The size of the assembled HTV was about the same size as the Pressurized Module of the Japanese Experiment Module “Kibo.” The HTV will be the largest payload that JAXA has ever launched.

    During the all-vehicle functional test, all the modules are mechanically and electrically connected to verify their function as one piece of the vehicle such as proper pipe routing and electric conductivity.

    The first HTV is scheduled to be launched by the H-IIB Launch Vehicle in September 2009 at the earliest.

    Aug. 28, 2008 Updated
    Thermal Vacuum Test for first flight of HTV

    A thermal vacuum test on the first flight vehicle of the H-II Transfer Vehicle (HTV) has been carried out at the Spacecraft Integration and Test Building at the Tsukuba Space Center.
    The purpose of the test is to evaluate the thermal design of the structure and to verify its endurance in the harsh environment of space by simulating the vacuum and thermal environment in space.
    Thermal vacuum tests for the Pressurized Carrier and Unpressurized Carrier have already been completed, and the main part with the Avionics Module and Propulsion Module combined is now in the 13-meter diameter space chamber for testing.
    The test will be completed in early September before the acoustic test and functional test are performed. After all the test results are reviewed to make sure that no problem is left unsolved, the vehicle will be transported to the Tanegashima Space Center for final launch preparations.

    (Photo: The main part of the HTV (Avionics Module and Propulsion Module) moved into the 13-meter diameter space chamber)

    Apr. 18, 2008 Updated
    The first model HTV (Technology Demonstration Model) was shown to the press

    On April 17, 2008, a press review was held for the first model H-II Transfer Vehicle (HTV) (Technology Demonstration Model), which is an unmanned cargo transfer spacecraft to the International Space Station. On display separately were the Pressurized Logistics Carrier for supply transportation, the Avionics Module for vehicle body control and the Propulsion Module which carries the propulsion system. When the HTV is completed and fully equipped, it will be the largest spacecraft in Japan with a length of 10 meters and a weight of 16.5 tons. After going through performance tests like the Thermal Vacuum Test and Acoustic Test, the first model HTV is scheduled for launch from Tanegashima on the H-IIB Launch Vehicle No. 1 (Test Model) in the summer of 2009.

    Jul. 2, 2007 Updated
    Proximity Communication System (PROX) undergoes testing

    Tests are currently being performed on the Proximity Communication System (PROX) at NASA’s Kennedy Space Center (KSC).

    The PROX system will be installed in the Japanese Experiment Module “Kibo” to communicate between the H-II Transfer Vehicle (HTV) and transmit and receive data between the International Space Station (ISS). It will also measure the relative distance and speed between the ISS and the HTV in order to support the HTV’s rendezvous with the ISS.

    Since last year, tests on the PROX and a compatibility test for the PROX/rack had been carried out before it went through a pre-shipping examination and was shipped out to the U.S. in January 2007. After performing several tests like the JEM/PROX compatibility test, it will be installed in the Experiment Logistics Module Pressurized Section (ELM-PS) and is scheduled for launch on Assembly Flight 1J/A at the end of February 2008.

    Photo1 : A general view of the PROX (Bottom right is the PROX before shipping at Tsukuba Space Center).
    Photo2 : A scene from a test on the PROX at the Kennedy Space Center.
    Photo3 : A crew review scene performed by astronaut Furukawa (taken from behind the PROX rack.)

    Jun. 26, 2006 Updated
    Prototype HTV unveiled to press at Tsukuba Space Center

    On June 23, a prototype of the H-II Transfer Vehicle (HTV) was unveiled to the press at the Tsukuba Space Center (TKSC.) The HTV is an unmanned orbital carrier to the International Space Station (ISS.) It is equipped with both the function of a “manned cargo carrier” for ISS crews to actually embark and carry out supportive work on it and the function of an “inter-orbital carrier” to perform “inter-orbit transportation to a selected attitude,” “rendezvous flights to the ISS,” and “re-entry” to aim to acquire the necessary technology for autonomous activities in space.

    The prototype will be used for various environment tests to make sure it can bear the extreme temperatures in space and acoustic and vibration environment at the time of launch. Through the tests, the project team will verify basic design data, and incorporate test results into future development.

    Outline of the HTV project

    Length about 10 m (including thruster)
    Diameter about 4.4 m
    Mass about 10.5 ton (excluding cargo)
    Loading capacity (for supply) about 6 tons
    Loading capacity (for waste) about 6 tons
    • Target orbit: ISS orbit
      Altitude: 350 to 460 km
      Inclination: about 51.6 degrees
    • Mission hours
      Solo flight: about 100 hours
      Stand-by: more than a week
      Docked with the ISS: about 30 days

    May 28, 2004 Updated
    Debris protection function was verified by shooting aluminum balls at the HTV at 6 km per second.

    Each module of the Space Station including the Japan Experiment Module has a “debris bumper” for protecting itself from losing its functions by colliding with space debris.
    The level of protection depends on the location (position) of each module and the probability of collision. Many technological ideas are incorporated to achieve the required protection effect, such as making the distance between the debris bumper and the pressurized wall longer.
    Solar array panels around the HTV have been considered to be part of the protective walls, but they needed to be verified.
    The verification was performed by a high-speed collision test using a HTV mockup. Aluminum balls of various sizes were shot at the protective walls at a speed of 6 km per second. After the test, the pressurized wall behind the protective walls was checked for holes. As a result, the solar array panels and the panel structure (an aluminum honeycomb structure) were verified to be effective for protection, and necessary data were also acquired for the further debris protection design assessment for the HTV.

    Upper Photo: A mockup for the verification (The thick wall on the right is a solar array panel.)
    Lower Photo:A solar panel from the back after the verification.

    Upper Photo: A mockup for the verification (The thick wall on the right is a solar array panel.)/Lower Photo:A solar panel from the back after the verification.;

    Mar. 28, 2003 Updated
    Manufacturing “Thermal Structural Test Models ” for Tests in the Next Fiscal Year

    HTV is about four meters in diameter and a bit shorter than 10 meters in length. In other words, its size can be explained as a container that could accommodate a sightseeing bus. In the process of developing HTV, therefore, it is divided into four modules namely Logistic Carrier Pressurized section, Logistic Carrier Un-Pressurized section, Avionics module, and Propulsion module. Thermal structural test models are being manufactured for each module. A thermal structural test model is a mimic model to test it in simulated harsh launch and space environments for checking acoustic condition, vibration, shock at separation and endurance in the space.

    The main structure is in conical semi-monocoque structure based on a launch vehicle design, and four modules will be assembled at the final fabrication phase and be tested for evaluating comprehensive strength and stiffness.

    Furthermore, tests for evaluating strength, pressure, acoustic data, shock, and heat balance, and acquisition of resonance frequency will be carried out to collect data for specifying environmental conditions of onboard loads and to find environmental characteristics data. The series of these tests will start in the next fiscal year.

    Upper Photo: Structural Thermal Test Model for Main Structure
    Lower Photo: Thermal Structural Test Model for Propulsion System “Helium Gas Supply Sub-Module”

    Oct. 5, 2001 Updated

    After HTV’s arrival to International Space Station (ISS), Exposed Pallet is taken out of HTV, and cargoes are replaced by robotic arm. This Exposed Pallet has rollers on its sides to minimize the friction and to keep the position accurately when it is brought back to HTV.
    A series of roller rotation slip tests was conducted from August to September 2001. The rollers are made of plastic to reduce the weight and they have solid lubricant on their surfaces. This combination of plastic and solid lubricant is rare. The purpose of this test is to confirm the manufacturing process and to collect the basic data of friction in the various environments (hot, cold, vacuum, air) and the wearing life.
    In addition, by conducting the test with the full-size model, the friction data closer to the actual operation were collected. The data will be applied not only for the HTV design and robotics analysis but also the future satellite programs and space equipment.

    Upper Photo: Setup for the rotation test in vacuum heat chamber
    Lower Photo: Setup for the full-size roller test

    Jun. 29, 2001 Updated

    Post Development Review of HTV Pressurized Carrier Aft Dome
    NASDA conducted additional preliminary design review (delta-PDR) with lots of participant from NASA and CSA (including ISS program manager) at Tsukuba Space Center as following schedule.
    Pre-Board Meeting : May 15th and 16th, 2001
    Board Meeting : May 18th, 2001
    We focused on two kinds of items in this review panel. One was a kind of additional items which were not reviewed in PDR held in 1999 (e.g.Un-pressurized carrier / Exposed pallet, GPS receivers in JEM, Crew operation panel, etc.) and another was a kind of items which had been changed the design from PDR (e.g. Solar power generation system, Approaching trajectory, etc.).
    Prior to holding the review panel, NASDA delivered review documents toward NASA, CSA and ESA and received a thousand of “Review Item Disposition Sheets (RID)” on these documents. We determined all dispositions for these RIDs after the discussions within three weeks. NASDA/NASA/CSA founded a few issues related to the ISS safety in this review panel and we determined to give high priority to these issues.

    Photo: HTV Delta-PDR Pre-Board Panel

    Feb. 19, 2001 Updated

    Post Development Review of HTV Pressurized Carrier Aft Dome A pressurized carrier equipped in HTV was designed based on the JEM Experiment Logistics Module Pressurized Section (ELM-PS). NASDA determined to use a newly designed integral molded structure for the Aft Dome of pressurized carrier to reduce the weight of 260 kg and the similar structure has already been used by the propellant tanks of Launch vehicles. Similar to H-IIA rocket, MAN-Technologie in Germany took the charge of the development under the supervision of Mitsubishi Heavy Industries LTD. Through this development, MAN-Technologie cleared the manufacturing problems such as thickness, welding, strength, etc., and completed them successfully. The photo shows a manufacturing sample that will be used for following engineering tests in Japan. After this review, NASDA will start manufacturing of the Flight Model and mass production.

    Photo: Aft Dome Structure for HTV Pressurized Carrier Engineering Test

    Dec. 8, 2000 Updated

    Succeeding to the previous tests conducted from April 18 to 20, 2000, NASDA/NASA/CSA conducted a series of real-time HTV capturing operation tests with expanded SSRMS conditions, evaluators, and facility by following schedule.
    Date: Nov. 8th to Nov. 10th, 2000
    Place: Canadian Space Agency Headquarter in Saint-Hubert, Quebec, CANADA
    In this series of tests, Astronaut Doi and other four astronauts executed total of up to 120 simulation- run cases with MOTS (MSS Operations and Training Simulator) in CSA, the facility with more complicated and numerous equipments. Just like previous tests, Astronauts evaluated the operability, by controlling SSRMS and executing capturing operation with free drifting HTV within predefined time. Though the results are still under investigation, the operation time was improved by re-designed operation sequence based on the experience in last tests.
    Photo (Upper): Astronaut Doi trying to capture Photo (Lower): CSA members supporting

    Nov. 9, 2000 Updated

    When crew enters HTV pressurized carrier berthed to ISS, it is necessary to circulate atmosphere in pressured cabin. The fan system for air circulation should meet several requirements such as large flow rate, low noise, lightweight, compact size, and high durability for severe environment during launch. Because each HTV mission period is relatively short, NASDA plans to develop a new air circulation fan system that is appropriate to HTV requirements.
    NASDA is conducting a series of development tests with this new fan system in Shinko-Denki Co. The purpose of tests is to ensure the silent and low vibration design with multi-stage/coaxial concept and new blade/housing shape. NASDA will then review the test results and reflect them to the final fan design.

    Photo: Test Setup

    Oct. 6, 2000 Updated

    The Pre-Shipping Review (PSR) for 28 R-1E thrusters, that will be used for HTV attitude control was held by Primex Space Systems Co. in the United States. These thrusters will be delivered to Ishikawajima-Harima Heavy Industries Co. Then after used in System Firing Test (SFT) in which NASDA confirms the Propulsion-system performance, they will be installed to the first HTV.
    The same thrusters have been used in Space Shuttle for attitude control and they will be installed in Propulsion Module of International Space Station.

    Photo: 28 sets of R-1E thruster (Offered by Primex Space Systems Co.)

    Jul. 7, 2000 Updated

    HTV has two carrier sections, one is a pressurized section which carries the logistics to ISS pressurized section and another is an un-pressurized section which carries experiment devices in ISS exposed section. The exposed experiment devices will be taken out from un-pressurized section with exposed pallet by ISS manipulator (SSRMS).
    From April 10 to June 8, NASDA had conducted Breadboard test in Mizuho facility of Ishikawajima-Harima Heavy Industries Ltd. for Paraffin Actuator that will be used for separation mechanism between exposed pallet and experiment devices. The Paraffin Actuator drives the output pin using phenomena of increasing of volume when paraffin changes its phases from solid to liquid and this attracts attention as a shock-less separation mechanism. In this series of tests, NASDA conducted a nominal driving test, environmental (vacuum/high temperature/low temperature) driving tests and a data-gathering test. NASDA obtained several data and the results will be used to improve the design of HCAM (HTV Cargo Attachment Mechanism).

    May 26, 2000 Updated

    HTV will perform autonomous rendezvous flight to the ISS, however, in the final operation, HTV will be captured by ISS manipulator system (SSRMS) controlled by ISS crew and be berthed to the ISS. Such operation is a peculiar requirement for HTV and we must confirm that it can be certainly captured by ISS crew within the limited time.
    To investigate the feasibility of this operation, a series of SSRMS capturing simulation test was conducted at MD-R (MacDonald Dettwiler Space and Advanced Robotics Limited) in Brampton City, Ontario, Canada from April 18 through 20. Besides four astronauts including Mr. Takao Doi, engineers from NASDA, CSA, and NASA had joined this test.
    In this simulation test, astronauts evaluated by controlling SSRMS and executing capturing operation in computer simulator: MDSF-RT (Manipulator Development and Simulation Facility in Real-Time) which HTV dynamics data from NASDA had been already input. Though details of the result are still under investigation, astronauts judged that this operation is feasible difficulty and it seemed that there are not any critical issues.

    Photo: HTV Capture Real-Time Crew Evaluation (offered by MD-R)

    Apr. 21, 2000 Updated

    In this month, NASA held the following safety review panel toconfirm the HTV safeness regarding to the International Space Station.
    HTV Safety Review Panel (Phase 1): March 13th to March 17th at Johnson Space Center in Houston.
    NASA holds the Safety Review Panel to all segments that compose the ISS and all approaching vehicles in rendezvousing to the ISS. Especially, HTV, which is the first newly designed transfer vehicle, turned out to be reviewed first in this panel. In this review panel, NASA and NASDA members had an animated discussion focused not only upon the hardware safety for the transfer vehicles such as logistics carrier and propulsion system but also upon the safety of flight-plan for rendezvous to the ISS. As a result, NASA confirmed the feasible of the HTV safety design and approved NASDA to progress the next design phase.

    Photo: Safety Review Panel Members

    Jan. 31, 2000 Updated

    PDR (Preliminary Design Review) for SIGI (Space Integrated GPSR/IMU) which is most important sensor of HTV Guidance and Navigation System was conducted at Honeywell co. in Tampa, Florida in United States from Dec. 9 to 10.
    In addition to accelerometers and ring laser gyros for control of HTV attitude/maneuver, this sensor unifies GPS receiver for navigation into one package.
    SIGI is also used in International Space Station to measure the attitude, and H764, the base of SIGI, are used in many aircraft.

    Figure: HTV Guidance and Control Schematic

    Dec. 17, 1999 Updated

    PDR (Preliminary Design Review) for Rendezvous Sensor which to be used during the HTV final approach was conducted at Daimler Chrysler Jena-Optronik in Jena, Germany from Nov.15 to 18. This sensor will also be used for ATV(Autonomous Transfer Vehicle) being developed by ESA.
    We expect a cost reduction / risk decrease become possible by this joint supply of NASDA-ESA.

    The figure: rendezous sensor function during final approach

    Nov. 19, 1999 Updated

    NASDA conducted the Approach/Release (Rendezvous) Flight Technology Test on the ETS-VII, which has close relation to the HTV rendezvous technology from Oct. 26 to 27.
    During the test, ETS-VII tried the R-bar approach which simulates the HTV final approach trajectory to the ISS. HIKOBOSHI satellite regarded as HTV, approached to the virtual R-bar formed by ORIHIME, using the algorithm developed for HTV. As a result, HIKOBOSHI raised the appropriate orbit within the expected corridor determined for rendezvous sensor and successfully finished at the 114 meters close.
    We are now analyzing the data obtained from this experiment. It will greatly contribute to the establishment of all HTV flight algorithm.

    Sep. 17, 1999 Updated

    NASDA held two major review meetings. One was the HTV Phase 1 Safety Review, which examined the HTV design from the point of safety. The another was HTV Preliminary Design Review (PDR), which examined the HTV design from the point of technique.
    The safety review meeting was held from August 18 to 20. The safety design of HTV was generally confirmed. After some additional study, HTV project will take a NASA safety review.
    The HTV PDR meeting was held by NASDA from August 23 to September 3. Approximately forty NASA, European Space Agency (ESA), and Canadian Space Agency (CSA) people attended the meeting and examined the HTV design. As the result of review, design of HTV was confirmed to be adequate. Therefore, the production of HTV Engineering Model (EM) and the progress to detailed design phase were admitted.

    Jul. 26, 1999 Updated

    The documents for PDR (Preliminary Design Review), which will be conducted from July 15th to September 3rd have been released. These documents have also been sent to NASA, CSA, and ESA in the end of June.
    We will continue to coordinate with reviewers of both NASDA and other organizations on matters which they point out until PDR Main Board.
    At the same time, the documents for Phase 1 Safety Review have been released.

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  • [Project Topics] KOUNOTORI5 launch postponed to Aug. 19 (Wed., JST)

    Topics List

    Aug. 17, 2015 Updated
    KOUNOTORI5 launch rescheduled to 8:50:49 p.m. on August 19 (Wed.) 2015

    The KOUNOTORI5(HTV5)/H-IIB F5 launch was postponed to 8:50:49 p.m. on August 19 due to adverse weather.
    Accordingly, the live launch report will begin at 8:00 p.m. on August 19 (Wed. , JST). The report will be broadcast through the Internet.
    Please send your support messages for the mission, or tweet it including the hashtag #HTV5.

    KOUNOTORI5 launch rescheduled to 8:50:49 p.m. on August 19 (Wed.) 2015

    Aug. 16, 2015 Updated
    KOUNOTORI5 launch postponed to Aug. 19 (Wed., JST)

    The launch date of the H-IIB Launch Vehicle No. 5 carrying the KOUNOTORI5 has been postponed as unfavorable weather is forecasted. The launch was originally scheduled for August 17. The live broadcast of the launch will also be put off accordingly.
    Your support messages are very much welcome through Twitter (Hashtag “#HTV5”) or via the following website.

    KOUNOTORI5 launch postponed to Aug. 19 (Wed., JST)

    Aug. 15, 2015 Updated
    New launch date and time of KOUNOTORI5/H-IIB F5 decided

    Aug. 14, 2015 Updated
    KOUNOTORI5 launch postponed to Aug. 17 (Mon., JST)

    The launch date of the H-IIB Launch Vehicle No. 5 carrying the KOUNOTORI5 has been postponed as unfavorable weather is forecasted. The launch was originally scheduled for August 16. The live broadcast of the launch will also be put off accordingly.
    Your support messages are very much welcome through Twitter (Hashtag “#HTV5”) or via the following website.

    KOUNOTORI5 launch postponed to Aug. 17 (Mon., JST)

    Jul. 21, 2015 Updated
    Dates set for capturing the KOUNOTORI5 and its berthing with ISS Astronaut Yui to be in charge of operation

    After international coordination, the dates for capturing the KOUNOTORI5, a cargo transporter to the International Space Station (ISS), and its berthing have been respectively set as August 20 (Thu.) and 21 (Fri.) The KOUNOTORI5 is scheduled to be launched on August 16 (Sun.) from the Tahegashima Space Center.
    It was also decided that Astronaut Kimiya Yui will manipulate the ISS robotic arm to capture the KOUNOTORI2.

    Dates set for capturing the KOUNOTORI5 and its berthing with ISS Astronaut Yui to be in charge of operation

    Jul. 10, 2015 Updated
    KOUNOTORI5 and operation simulation training opened to the press

    On July 1, the KOUNOTORI5, a cargo transporter to the ISS, was revealed to the media at the Tanegashima Space Center. The mission was also explained there.
    From the evening of July 9 to the morning of the 10th, simulation training for the KOUNOTORI5 operation and control was held in the KOUNOTORI operation room at the Tsukuba Space Center, and part of it was also open to the press. This training was a last opportunity for a joint session between JAXA and NASA before the KOUNOTORI5 launch. On the NASA side, Astronaut Wakata participated in the training as a CAPCOM (capsule/spacecraft communicator).

    KOUNOTORI5 and operation simulation training opened to the press

    Jun. 9, 2015 Updated
    Launch day set for KOUNOTORI5/H-IIB F5!

    The launch date and time for the H-IIB Launch Vehicle No. 5 (H-IIB F5) with the H-II Transfer Vehicle “KOUNOTORI5” (HTV5) onboard was set for around 10:01 p.m. on August 16 (Sun.), 2015 (Japan Standard Time).
    The H-IIB F5 has already been transported to the TNSC, and it is now being assembled there.
    * Launch time will be determined by the updated orbit of the ISS.

    Launch day set for KOUNOTORI5/H-IIB F5!

    Sep. 7, 2013 Updated
    KOUNOTORI4 completed its mission with re-entry!

    The KOUNOTORI4 (HTV4, a cargo transporter to the International Space Station) left the ISS on Sept. 5 and re-entered the atmosphere at 3:37 p.m. on Sept. 7 (Japan Standard Time.)
    The KOUNOTORI 4 successfully achieved its mission of taking cargo to the ISS, then completed all its tasks over about 36 days.
    We would like to send our sincere appreciation to all of you who have been supporting the KOUNOTORI project.

    KOUNOTORI4 completed its mission with re-entry!

    Sep. 3, 2013 Updated
    Re-entry date and time for KOUNOTORI4 decided

    Schedules of departure from the International Space Station (ISS) and of re-entry to the atmosphere for the H-II Transfer Vehicle “KOUNOTORI 4” (HTV4) are determined as follows.

    Departure from the ISS:
    September 5, 2013 / 1:00 a.m.(Japanese Standard Time, JST)*
    Re-entry to the atmosphere:
    September 7, 2013 / 3:36 p.m.(JST)*

    * The time may vary according to the actual operation.

    Aug. 10, 2013 Updated
    KOUNOTORI4 berthed at ISS!

    The KOUNOTORI4 (HTV4, a cargo transporter to the International Space Station) was captured by the ISS robotic arm at 8:22 p.m. on August 9 (Japan Standard Time) and berthed at the ISS at 3:38 a.m. on August 10 (JST). The KOUNOTORI4 was launched by the H-IIB Launch Vehicle No.4 on August 4. ISS astronauts will take cargo out from the Pressurized and Unpressurized Logistic Carriers into the ISS.

    Aug. 9, 2013 Updated
    Live broadcast of KOUNOTORI4 trip to ISS!

    The KOUNOTORI3 (HTV4, the cargo transporter to the International Space Station) launched on August 4 has been traveling to the ISS while adjusting its altitude. Between the evening on August 9 and early on the morning of August 10, the KOUNOTORI4 will make a final approach and berth at the ISS. JAXA will provide a live broadcast of its final access, capture, and berthing.
    The KOUNOTORI4’s approach and the ISS’s capture of the vehicle by the robotic arm is scheduled for about one hour from 7:40 p.m. on the 9th (Japan Standard Time.) Then the telecast of its berthing will last for about one hour from 22:00 p.m. on the 9th (JST.)
    Please don’t miss the broadcast!
    (Photo: The KOUNOTORI3 approaching the ISS, JAXA/NASA)

    Aug. 4, 2013 Updated
    Launch Success of KOUNOTORI4/H-IIB F4

    The H-IIB Launch Vehicle No. 4 with the KOUNOTORI4 (HTV4, a cargo transporter to the International Space Station) onboard lifted off from the Tanegashima Space Center at4:48:46 a.m. on August 4 (Sun., Japan Standard Time.)
    The launch vehicle flew smoothly, and at 14 minutes and 59 seconds after liftoff, the KOUNOTORI4 separation was confirmed.
    The KOUNOTORI4 will gradually go closer to the International Space Station, and it will be berthed at the ISS. We will broadcast the berthing on our website, so don’t miss it!

    Jun. 19, 2013 Updated
    KOUNOTORI4 revealed at TNSC

    On June 19, the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) “KOUNOTORI4” was shown to the media at the Tanegashima Space Center (TNSC.)
    The KOUNOTORI4 will be launched by the H-IIB Launch Vehicle No. 4 on Aug. 4 from the TNSC. It will carry various goods to the ISS including food and water for astronauts, as well as experiment devices and materials for the Japanese Experiment Module “Kibo.” Launch preparations continue for the KOUNOTORI4.

    May 21, 2013 Updated
    KOUNOTORI4/H-IIB F4 launch schedule decided!

    The H-IIB Launch Vehicle No. 4 (H-IIB F4) carrying the H-II Transfer Vehicle (HTV4, a cargo transporter to the International Space Station) will be launched on August 4 (Sunday, Japan Standard Time.) The launch time will be around 4:48 a.m. (JST.) It will be blasted off from the Yoshinobu Launch Complex at the Tanegahsima Space Center. Why don’t you take this opportunity to come to Tanegahima to witness the liftoff at hand!

    Sep. 14, 2012 Updated
    KOUNOTORI3 completed its mission with re-entry!

    The KOUNOTORI3 (HTV3, a cargo transporter to the International Space Station) left the ISS on Sept. 13 and re-entered the atmosphere at 2:27 p.m. on Sept. 14 (Japan Standard Time.)
    The KOUNOTORI 3 successfully achieved its mission of taking cargo to the ISS, then completed all its tasks over about 56 days.
    We would like to send our sincere appreciation to all of you who have been supporting the KOUNOTORI project.

    Sep. 11, 2012 Updated
    KOUNOTORI3 departure and re-entry live report!

    The H-II Transfer Vehicle “KOUNOTORI3” (HTV3,a cargo transporter to the International Space Station) will leave from the ISS at around 0:50 a.m. on Sept. 13 (Japan Standard Time, all the following dates and time are JST,) and will re-enter the atmosphere at around 2:24 p.m. on Sept. 14.
    JAXA will offer a live report of its departure from the ISS from 0:20 a.m. on the 13th (Thu.), then a live scene of the HTV operation room at the time of its re-entry from 1:45 p.m. on the 14th (Fri.) through the Internet. Please do not miss the footage!

    Sep. 7, 2012 Updated
    Re-entry date and time for KOUNOTORI3 decided

    The re-entry schedule for the KOUNOTORI3 was set as follows after extended mooring at the International Space Station due to an additional extravascular activity.

    Departure from the ISS:
    September 13, 2012 / 0:50 a.m.(Japanese Standard Time, JST)*
    Re-entry to the atmosphere:
    September 14, 2012 / 2:24 p.m.(JST)*

    * The time is subject to change due to actual operational status.

    The KOUNOTORI3 will carry a re-entry data recorder, the i-Ball, which was developed in cooperation between the public and private sectors to acquire atmosphere re-entry data as well as scenes of KOUNOTORI3’s destruction.

    Jul. 28, 2012 Updated
    KOUNOTORI3 berthed at ISS!

    The KOUNOTORI3 (HTV3, a cargo transporter to the International Space Station) was captured by the ISS robotic arm at 9:23 p.m. on July 27 (Japan Standard Time) and berthed at the ISS at 2:31 a.m. on July 28. The KOUNOTORI3 was launched by the H-IIB Launch Vehicle No.3 on July 21. ISS astronauts will take cargo out from the Pressurized and Unpressurized Logistic Carriers into the ISS.
    (Photo: The KOUNOTORI3 to a Common Berthing Mechanism at the nadir port of Harmony, JAXA/NASA)

    Jul. 21, 2012 Updated
    Launch Success of KOUNOTORI3/H-IIB F3

    The H-IIB Launch Vehicle No. 3 with the KOUNOTORI3 (HTV3, a cargo transporter to the International Space Station) onboard lifted off from the Tanegashima Space Center at 11:06:18 on July 21 (Sat., Japan Standard Time.)
    The launch vehicle flew smoothly, and at 14 minutes and 53 seconds after liftoff, the KOUNOTORI3 separation was confirmed.
    The KOUNOTORI3 will gradually go closer to the International Space Station, and it will be berthed at the ISS. We will broadcast the berthing on our website, so don’t miss it!

    Jun. 21, 2012 Updated
    KOUNOTORI3/H-IIB F3 Special Site now open!

    JAXA will launch the KOUNOTORI3 (a cargo transporter to the International Space Station, ISS) by H-IIB Launch vehicle No.3 on July 21 from the Tanegashima Space Center. We have opened the KOUNOTORI3/H-IIB F3 Special Site to be ready for the launch.
    Please check the special site for more information. We have also started welcoming your support messages, so please send them to us!

    Jun. 7, 2012 Updated
    KOUNOTORI3 revealed to the media at TNSC

    On June 1 (Fri.), the H-II Transfer Vehicle “KOUNOTORI3” (HTV3, a cargo transporter to the International Space Station) was revealed to the media at the Spacecraft and Fairing Assembly Building 2 at the Tanegashima Space Center. The KOUNOTORI3 will be packed with food and daily necessities for astronauts aboard the ISS, test equipment for aquatic organisms, and other experiment devices including a small satellite, then will be launched by the H-IIB Launch Vehicle No. 3 at 11:18 a.m. on July 21, 2012 (Japan Standard Time.) The KOUNOTORI is currently under preparations for its journey to space.

    Mar. 21, 2012 Updated
    KOUNOTORI3/H-IIB F3 launch schedule decided!

    The launch date and time for the H-IIB Launch Vehicle No. 3 (H-IIB F3) with the H-II Transfer Vehicle “KOUNOTORI3” (HTV3), a cargo transporter to the International Space Station, has been set to be at around 11:18 a.m. on July 21 (Sat.), 2012 (Japan Standard Time.) The launch preparation operation for the KOUNOTORI is smoothly in progress at the Tanegashima Space Center.

    Mar. 30, 2011 Updated
    KOUNOTORI2 re-entered the atmosphere to complete its mission!

    The KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station,) which left the ISS at around 0:46 a.m. on March 29 (Japan Standard Time,) re-entered the atmosphere at around 12:09 p.m. on March 30 (JST.)
    The KOUNOTORI2 successfully completed its role to transport materials to the ISS, then re-entered the Earth’s atmosphere to complete its mission of approximately 67 days.
    Thank you very much for supporting the KOUNOTORI2 and H-IIB Launch Vehicle No.2 missions.

    Mar. 29, 2011 Updated
    KOUNOTORI2 left ISS!

    The KOUNOTORI2 (HTV2, a cargo transporter to the ISS) was detached from the International Space Station (ISS) using the ISS robotic arm at 10:29 p.m. on March 28 (Japan Standard time,) and it emitted a jet to leave the ISS after being transported to the release point at 0:46 a.m. on the 30th.
    The KOUNOTORI2 will re-enter the Earth’s atmosphere at around 12:09 on March 30. From some areas, you can see the KOUNOTORI2 flying around the Earth between the 29th and the 30th. Also, please witness the scene of the HTV operation and control room when it re-enters the atmosphere through the live Internet broadcast, which will begin at 11:30 a.m. on the 30th.

    Mar. 25, 2011 Updated
    KOUNOTORI2 leaving ISS on the 29th! Live broadcast scheduled

    The KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station) will depart from the ISS with used material loaded on March 29 (Japan Standard Time,) and will be slated for re-entry to the atmosphere on the 30th (JST.) JAXA will broadcast a live Internet report of the KOUNOTORI departure from the ISS from 0:00 a.m. on the 29th (JST,) then its re-entry to the atmosphere from 11:30 a.m. on the 30th (JST.) Please watch the events through the Internet!

    Mar. 22, 2011 Updated
    KOUNOTORI2 to leave ISS

    The departure date of the KOUNOTORI2 (HTV2, a cargo transporter to the ISS), which is loaded with used materials, from the International Space Station (ISS) has been decided.
    The KOUNOTORI2 will leave the ISS at around 0:45 a.m. on March 29 (Japan Standard Time) after completing its role at the ISS. After departure, it will be burned when it re-enters the atmosphere at around 12:10 p.m. on March 30. Following its combustion, its mission will be accomplished.
    We will broadcast a live report of the departure and re-entry of the KOUNOTORI2. More details will be posted on our website. (Photo by NASA)

    Mar. 11, 2011 Updated
    KOUNOTORI2 relocation to the earth-facing port completed

    At 8:49 p.m. on March 10 (Japan Standard Time), the KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station) began to be moved from the zenith port to the earth-facing port using the robotic arm of the International Space Station. At 3:55 a.m. on the 11th (JST,) KOUNOTORI2’s electric and communication systems were connected to the ISS to complete the relocation. After being loaded with used items, the KOUNOTORI2 will re-enter the atmosphere to be burned.

    Mar. 9, 2011 Updated
    KOUNOTORI2 to return to earth-facing port from March 10

    The KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station), will move back to the earth-facing port of the Harmony (Node 2) from its zenith port now that the Space Shuttle Discovery left the ISS to go home on March 7 (Japan Standard Time.) The relocation is scheduled to be performed on the 10th and 11th (JST.) More cargo will be taken out of the KOUNOTORI2, then, after being packed with used materials, the KOUNOTORI2 will re-enter the atmosphere.
    (Photo by NASA)

    Feb. 21, 2011 Updated
    KOUNOTORI2 relocation to the zenith port completed

    As part of preparations for the Space Shuttle Discovery’ s docking with the International Space Station (ISS,) the KOUNOTORI2 , or the HTV2, a cargo transporter to the ISS, was moved from the earth-facing port of the Harmony (Node 2) to its zenith port. This was the first time to perform such a relocation. The KOUNOTORI2 was successfully transported at 1:45 a.m. on Feb. 19 (Japan Standard Time,) and the electric cables were connected with the Harmony at 4:26 a.m. (JST) to complete its relocation.

    Jan. 28, 2011 Updated
    KOUNOTORI2 berthing at ISS

    The KOUNOTORI2, or the HTV2, a cargo transporter to the International Space Station (ISS) launched by the H-IIB Launch Vehicle No.2, was captured by the ISS robotic arm at around 8:41 p.m. on January 27 (Japan Standard Time,) and, at around 3:34 a.m. on the 28th (JST,) the KOUNOTORI berthed at the ISS. Cargo in the Pressurized Section will be transported to the ISS by the ISS astronauts followed by cargo in unpressurized areas.

    Jan. 22, 2011 Updated
    KOUNOTORI2/H-IIB F2 successfully launched

    The H-IIB Launch Vehicle No. 2 with the KOUNOTORI2 (HTV2, a cargo transporter to the International Space Station, ISS) onboard was launched from the Tanegashima Space Center at 2:37:57 p.m. on January 22 (Sat., Japan Standard Time.) The launch vehicle flew smoothly, and, at about 15 minutes and 13 seconds after liftoff, the separation of the KOUNOTORI2 was confirmed.
    The KOUNOTORI2 will fly to the ISS, then, on Jan. 28 (Fri., JST,) it is slated for berthing with the ISS.

    Dec. 14, 2010 Updated
    KOUNOTORI2 system checkup completed

    At the Tanegashima Space Center, all parts of the H-II Transfer Vehicle “KOUNOTORI2” (HTV2) were integrated electrically and mechanically in the end of October. Throughout November, the assembled KOUNOTORI2 has been checked as one system to confirm that no problem was found in the vehicle.
    After a thorough inspection, propellants were loaded onto the KOUNOTORI2 tanks, and currently the tank pressure is being adjusted. Preparation for launch is smoothly progressing.
    The final launch preparation including battery charge and loading onto the H-IIA Launch Vehicle No.2 will now be carried out for the KOUNOTORI2.

    Dec. 1, 2010 Updated
    KOUNOTORI2 control and operation simulation revealed to the press

    On November 30, JAXA showed part of the control and operation simulation of the KOUNOTORI2 to the media at the Tsukuba Space Center. The KOUNOTORI2 (HTV2) is a cargo transfer vehicle to the International Space Station (ISS.)
    The purpose of the simulation was to train and improve operators’ skills. It takes about 20 hours with NASA to simulate events, from the KOUNOTORI2’s arrival at around 12-km beneath the ISS, to its gradual approach to the ISS, to the capture of the KOUNOTORI2 by the ISS robotic arm, and then the docking of the KOUNOTORI2.

    Nov. 26, 2010 Updated
    KOUNOTORI2 shown to the Press at TNSC

    On Nov. 25, the H-II Transfer Vehicle “KOUNOTORI”2 (a cargo transporter to the International Space Station) was revealed to the media at the Spacecraft and Fairing Assembly Building No. 2 at the Tanegashima Space Center. We are engaging in preparation for the launch of the KOUNOTORI2 including propellant loading and mating with the launch vehicle.
    JAXA provides updated information about the KOUNOTORI2 and H-IIB Launch Vehicle No.2 at the special site. Your support messages are welcome there, too.

    Nov. 11, 2010 Updated
    HTV nickname selected & special site open!

    “KOUNOTORI” (meaning “a white stork” in English) was chosen as the nickname of the H-II Transfer Vehicle (HTV, a cargo transfer vehicle to the International Space Station.)
    During a month-long nickname campaign, we received 17,236 suggestions.
    Among them, “KOUNOTORI” was selected because a white stork carries an image of conveying an important thing (a baby, happiness, and other joyful things); therefore, it precisely expresses the mission to transport essential materials to the ISS.
    The KOUNOTORI2 is scheduled to be launched by the H-IIB Launch Vehicle No. 2 (H-IIB F2) at around 3:29 p.m. (Japan Standard Time) on January 20 (Thu.), 2011.
    Taking this opportunity of selecting the nickname, we would also like to open the “KOUNOTORI2/H-IIB F2 Special Site.” We will provide you with updated information about the project including a column by project personnel and launch related matters. Please enjoy the site!
    * Launch time will be determined by the updated orbit of the ISS.

    Nov. 10, 2010 Updated
    Launch day set for HTV2/H-IIB F2!

    The launch date and time for the H-IIB Launch Vehicle No. 2 (H-IIB F2) with the H-II Transfer Vehicle (HTV2) onboard was set for around 3:29 p.m. on January 20 (Thu.), 2011 (Japan Standard Time). The HTV2 is a cargo transporter to the International Space Station (ISS.) The integration of all modules of the HTV2 was completed at the Tanegashima Space Center (TNSC), and it will enter the final launch preparation phase. The H-IIB F2 has already been transported to the TNSC, and it is now being assembled there.
    * Launch time will be determined by the updated orbit of the ISS.

    Nov. 2, 2010 Updated
    HTV2: all modules connected, moved to final launch preparations

    (Left) All HTV2 modules are being connected (Center) Integrated HTV2 (front side) (Right) Integrated HTV2 (back side) (Images by JAXA)

    On Oct. 29, we completed connecting all modules of the second H-II Transfer Vehicle (HTV2, a cargo transporter to the International Space Station) electrically and mechanically at the Second Spacecraft and Fairing Assembly Building (SFA2) at the Tanegashima Space Center. The HTV2 is now in its configuration for launch.
    After a comprehensive check on the integrated HTV2, it will go through final launch preparations including propellant loading and fairing encapsulation. The HTV2 is scheduled to be launched in the winter launch period of Japan Fiscal Year 2010.

    Oct. 13, 2010 Updated
    Full assembly started for the second HTV

    The assembly operation for all modules of the second H-II Transfer Vehicle (HTV, the cargo transporter to the International Space Station) started on October 6 at the second Spacecraft and Fairing Assembly Building (SFA2) at the Tanegashima Space Center. Prior to full assembly, in mid September, cargo to the ISS was loaded onto the Pressurized and Unpressurized Carriers.

    Apr. 7, 2010 Updated
    Development of HTV/H-IIB received Japan industry technology/MEXT award

    JAXA was selected as one of 12 organizations to receive the Ministry of Education, Culture, Sports, Science and Technology award at the 39th Japan industry technology awards for its development of the HTV and H-IIB launch vehicle.
    The Japan industry technology awards are presented by Nikkan Kogyo Shimbun Ltd. (Business and Technology Daily News, Japan) to encourage development of original and unique technology that contributes to the promotion of industry. The news company bestows the awards to development projects of distinctive large-scale technological systems.

    Feb. 10, 2010 Updated
    HTV Project Team awarded for research

    Since 2005, the National Institute of Science Technology Policy (NISTEP) of the Ministry of Education, Culture, Sports, Science and Technology (MEXT) has been choosing researchers who have made significant contributions to science and technology every year to praise their efforts. In 2009, the demonstration flight of the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) was highly evaluated, and on February 9, Mr. Torano, HTV Project Manager, Mr. Koyari, Sub-project Manager, and Mr. Sasaki, Functional Manager, received a memento of the selection.

    Nov. 2, 2009 Updated
    HTV re-entered the atmosphere, mission completed

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which departed from the International Space Station (ISS) on October 31, re-entered the atmosphere at around 6:26 a.m. on November 2.
    The HTV successfully completed its cargo transportation operations to the ISS, and accomplished all its missions in about 52 days following the re-entry today.

    Oct. 31, 2009 Updated
    HTV released from ISS

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which completed its cargo transportation mission at the International Space Station (ISS), was unberthed from the ISS by its robotic arm (SSRMS) at 0:02 a.m. on October 31 (Japan Standard Time, the following dates and times are JST.) The HTV departed from the ISS at 2:32 a.m. on the 31st. The HTV will leave the ISS orbit, and is scheduled to re-enter the Earth’s atmosphere at around 6:25 a.m. on November 2 (Mon.)
    You may be able to see the HTV just prior to re-entry from Okinawa at around 6:13 a.m. on the 2nd if the deorbit process goes smoothly and the weather cooperates. (Photo by NASA)

    Oct. 27, 2009 Updated
    Internet Live Report: HTV leaving ISS on Oct. 31 (Sat)

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which is currently berthed at the International Space Station (ISS), is scheduled to depart from the ISS at 2:30 a.m. on Oct. 31 (Sat) (Japan Standard Time, all the following days and times are in JST.) The HTV will be unberthed from the ISS by the ISS robotic arm (SSRMS) late at night on Oct. 30 (Fri) after its hatch to the ISS is closed at dawn of Oct. 30, then depart from the ISS. If everything goes smoothly, the HTV will re-enter the Earth’s atmosphere around 6:25 a.m. on Nov. 2 (Mon).

    We will broadcast a live report of the HTV unberthing and departure from the ISS through the Internet from 11:45 p.m. on Oct. 30 (Fri) and from 2:15 a.m. on Oct. 31 (Sat) respectively. (Sorry, the live reports are broadcasted only in the Japanese language.) Please enjoy the HTV live reports over the weekend!
    The live broadcast time schedule has changed due to the delay of the HTV departure.

    Oct. 21, 2009 Updated
    The HTV PLC unloading operations completed, trash loading continues

    HTV-1, being berthed to the ISS, is operating nominally. The Small Fine Arm (SFA) of the Kibo Remote Manipulator System (JEMRMS), packed in a Cargo Transfer Bag (CTB) and delivered to the ISS, was transferred from the HTV Pressurized Logistics Carrier (PLC) to Kibo on October 4. The Pressurized Stowage Resupply Rack (PSRR), also delivered on the HTV-1, was transferred to Kibo’s Experiment Logistics Module-Pressurized Section (ELM-PS) on October 14. All the cargo transfer operation from the HTV PLC to the ISS was completed on October 20.
    Aboard the ISS, trash loading into the HTV PLC is currently underway. With this trash stow activity completed, the HTV-1 will depart from the ISS, and enter the atmosphere early next month.
    Photo (provided by NASA): Astronaut Robert Thirsk taking cargo out from the HTV Pressurized Carrier.

    Oct. 14, 2009 Updated
    HTV operations running smoothly, cargo unloading continues

    Cargo unloading operations continued from the Pressurized Logistics Carrier of the H-II Transfer Vehicle (HTV) Demonstration Flight berthed at the International Space Station (ISS). On Oct. 4, the Small Fine Arm (SFA) of the Kibo’s Robotic Arm was moved to the ISS. The SFA was transported to the ISS as it was still packed in the Cargo Transfer Bag. One unit of the Pressurized Stowage Resupply Rack will be transferred to the ISS on the 14th.
    Photo (provided by NASA): Astronaut Nicole Stott taking cargo out from the HTV Pressurized Carrier.

    Sep. 26, 2009 Updated
    Exposed Pallet stored back in HTV

    The Exposed Pallet of the H-II Transfer Vehicle (HTV) Demonstration Flight was retrieved and stored back in the HTV Unpressurized Carrier at 10:20 p.m. on Sept. 25 (Japan Standard Time) by the robotic arms of the Kibo and the International Space Station (SSRMS) after its two cargoes, the experiment devices in the unpressurized environment, had been installed in the Kibo’s Exposed Facility.
    Cargo in the HTV Pressurized Carrier will now be unloaded by the astronauts aboard the ISS. After the unloading, used material and equipment on the ISS will be packed into the Pressurized Carrier. The HTV will depart from the ISS in mid-November to re-enter the atmosphere. (The detailed schedule will be decided based on the ISS/HTV operational status.) (Photo by NASA)

    Sep. 25, 2009 Updated
    Two experiment devices installed onto Kibo Exposed Facility

    On Sept. 24 and 25 (Japan Standard Time), two experiment devices that were shipped by the H-II Transfer Vehicle (HTV) Demonstration Flight were unloaded from the HTV Exposed Pallet and installed onto the Exposed Facility of the Japanese Experiment Module “Kibo.”
    The two devices are the “Superconducting Submilimeter-Wave Limb-Emission Sounder (SMILES)” and the “Hyperspectral Imager for the Coastal Ocean (HICO) & Remote Atmospheric & Ionospheric Detection System (RAIDS) Experimental Payload (HREP.)” The HREP and the SMILES were mounted at 8:15 p.m. on the 24th and 1:12 a.m on the 25th respectively. (Photo by NASA)

    Sep. 24, 2009 Updated
    HTV Exposed Pallet attached to the Kibo Exposed Facility

    At 6:06 p.m. on Sept. 23rd (Japan Standard Time, JST), the Exposed Pallet was taken out from the H-II Transfer Vehicle (HTV) Demonstration Flight, which is now berthed at the International Space Station (ISS). The Pallet was then attached onto the Exposed Facility of the Japanese Experiment Module “Kibo” at 11:33 p.m. (JST). The experiment devices on the Pallet will be moved to be installed onto the Kibo’s Exposed Facility. (Photo by NASA)

    Sep. 18, 2009 Updated
    HTV Demonstration Flight successfully berthed at ISS

    The H-II Transfer Vehicle (HTV) Demonstration Flight, launched by the H-IIB Launch Vehicle Test Flight at 2:01 a.m. on Sept. 11 (Japan Standard Time, JST,) took almost one week to approach the International Space Station (ISS) and arrived at the Berthing Point 10 meters below the ISS at 4:27 a.m. on the 18th (JST, following times are all JST.) At 4:51 a.m., the HTV was captured by the ISS robotic arm (Space Station Remote Manipulator System, SSRMS) manipulated by the ISS crew, and it was installed onto the Common Berthing Mechanism (CBM) on the lower side (earth side) of the Harmony (Node 2) at 7:26 a.m. At 10:49 a.m., electric and communication lines were connected, and the HTV was successfully berthed at the ISS.

    Sep. 15, 2009 Updated
    Live reports of the HTV final approach to the ISS on Sept. 18 (Fri.)

    The H-II Transfer Vehicle (HTV) Demonstration Flight, which was launched by the H-IIB Launch Vehicle at 2:01:46 a.m. on September 11 (Fri.) has been smoothly flying on its scheduled course. Its final approach to the International Space Station (ISS) was approved at the ISS Mission Management Team (IMMT) meeting on Sept. 15, thus, from the 16th, the altitude of the HTV will be maneuvered to gradually approach the ISS. The HTV is scheduled to be berthed at the ISS on Sept. 18 (Fri.)
    JAXA will broadcast the live reports of the ISS robotic arm capturing the HTV from 4:00 a.m., and the berthing of the HTV at the ISS from 7:00 a.m. They are early in the morning, but don’t miss them!

    Sep. 11, 2009 Updated
    HTV/H-IIB Successfully Launched!!

    The Japan Aerospace Exploration Agency (JAXA) launched the H-II Transfer Vehicle (HTV) Demonstration Flight aboard the H-IIB Launch Vehicle Test Flight (H-IIB TF1) at 2:01:46 a.m. on September 11, 2009 (Japan Standard Time, JST) from the Tanegashima Space Center. The launch vehicle flew smoothly, and, at about 15 minutes and 6 seconds after liftoff, the separation of the HTV Demonstration Flight was confirmed.

    The HTV will gradually approach the International Space Station (ISS) and berth at the ISS on the 18th (Friday, JST.)

    Aug. 31, 2009 Updated
    HTV moved to the VAB! Final launch preparation phase

    On August 30, the encapsulated HTV Demonstration Flight was transported to the Vehicle Assembly Building (VAB.) It will be loaded onto the H-IIB Launch Vehicle to be ready for the launch on September 11. We published a promotion movie of the HTV/H-IIB mission. Please watch it before witnessing the actual launch!

    Aug. 24, 2009 Updated
    HTV encapsulated

    On August 21, the H-II Transfer Vehicle (HTV) Demonstration Flight was mated with the Payload Attach Fitting (PAF) at the Spacecraft and Fairing Assembly Building #2.
    On the 23rd, the HTV on the PAF was encapsulated by the payload fairing, which covers the payload to protect it from air resistance, friction and the acoustic vibrations of launch. The fairing for the HTV is a 5S-H type and is about 5 meters in diameter and about 15 meters in length. It was developed for the HTV launch.
    The encapsulated HTV Demonstration Flight will be transported to the Vehicle Assembly Building (VAB) and loaded onto the H-IIB Launch Vehicle Test Flight.

    Jul. 9, 2009 Updated
    HTV opened to the press at TNSC

    On July 9, the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) was opened to the press at the Spacecraft and Fairing Assembly Building #2 (SFA2) at the Tanegashima Space Center (TNSC.)
    We are providing updated information on the HTV and H-IIB at the HTV/H-IIB Special Site.

    Jul. 8, 2009 Updated
    HTV/H-IIB launch date decided! Special site opened

    The H-IIB Launch Vehicle Test Flight with the H-II Transfer Vehicle (HTV, a cargo transporter to the International Space Station) will be launched at 2:04 a.m. on September 11 (Fri.). (*)
    The HTV has been fully assembled at the Tanegashima Space Center, and it will be under final launch preparations including comprehensive checkout and propellant loading to be ready for launch.
    The ground comprehensive test for the H-IIB Launch Vehicle using the Ground Test Vehicle (the GTV test) is scheduled on the 11th.
    Please check the updated information on the HTV and H-IIB at the “HTV/H-IIB Special Site,” which was opened today. We hope you enjoy the site.
    (*) Time will be determined by the updated orbit of the International Space Station (ISS.)

    Jun. 30, 2009 Updated
    Preparations for the HTV Demonstration Flight going smoothly at TNSC

    Preparations for the Demonstration Flight of the H-II Transfer Vehicle (HTV) are underway at the Tanegashima Space Center (TNSC).
    At dawn on April 23, the HTV arrived at the TNSC and was moved into the Spacecraft and Fairing Assembly Building #2 for a post-transportation inspection on each element of the vehicle.
    Payloads to be shipped to the International Space Station (ISS) by the HTV were then loaded onto the HTV’s Pressurized Logistic Carrier and Unpressurized Logistic Carrier.

    In the Pressurized Logistic Carrier, life-related supplies, such as food and clothes, which were packed in the Cargo Transfer Bag (CTB) and other experiment materials were stored on the HTV Re-supply Rack (HRR) of the Carrier. In the Unpressurized Logistic Carrier, the Superconducting Submilimeter-Wave Limb-Emission Sounder (SMILES,) which is an experiment device for the Kibo’s Exposed Facility, and NASA experimental equipment were loaded onto the Exposed Pallet of the Carrier.

    After completing the payload loading, the two carriers were mated.
    On June 24, all HTV modules including the Avionics Module and Propulsion Module were connected.
    The HTV demonstration flight is now fully assembled, and will start final launch preparations such as a comprehensive vehicle inspection and propellant loading.

    Apr. 24, 2009 Updated
    HTV arrives at TNSC

    At dawn on April 23, the First H-II Transfer Vehicle (HTV) was transported from Shimama Port at Tanegashima to the Tanegashima Space Center (TNSC.) The HTV left the Tsukuba Space Center on April 17. The Pressurized Logistic Carrier, Unpressurized Logistic Carrier, the Avionics Module, and the Propulsion Module were detached for the transportation, thus they will be assembled after arrival. A final functional checkup will be held prior to the launch.

    Apr. 17, 2009 Updated
    HTV left for the TNSC

    The first H-II Transfer Vehicle (HTV), or the HTV Technology Demonstrator, left the Tsukuba Space Center at dawn on April 17, 2009, for the Tanegashima Space Center (TNSC.) After arrival, the HTV will be assembled and checked for launch by the H-IIB Launch Vehicle, which is now under testing.


    The first HTV leaving the TKSC (Unpressurized Logistics Carrier, Avionics Module, and Plopulsion Module)

    The first HTV arrived at Tsuchiura Port
    (Unpressurized Logistics Carrier)

    Dec. 26, 2008 Updated
    HTV open to the press

    On Dec. 25, 2008, JAXA revealed the maiden H-II Transfer Vehicle (HTV), an unmanned supply transfer vehicle that will fly to the International Space Station (ISS), to the press at the Tsukuba Space Center (TKSC.) It was the first press conference since assembling all the modules of the first HTV.

    At the press conference, the HTV and its launch by the H-IIB Launch Vehicle were explained by HTV Project Manager Yoshihiko Torano and H-IIB Launch Vehicle Project Manger Tomihisa Nakamura. The Superconducting Submilimeter-Wave Limb-Emission Sounder (SMILES,) which will be transported to the ISS by the first HTV, was also introduced by Professor Masato Shiotani of the Research Institute for Sustainable Humanosphere of Kyoto University. The SMILES is one of the experiment devices that will be installed onto the Exposed Facility of the Japanese Experiment Module “Kibo.”

    Also at the press conference, the first HTV and the SMILES undergoing an all-vehicle functional test were shown to the media at the Spacecraft Integration and Test Building at the TKSC. The modules of the cargo section (“Pressurized Carrier” and “Unpressurized Carrier,”) “Avionics Module” and “Propulsion Module” were assembled for the test. The “Exposed Pallet” loaded with a dummy cargo for the test and the SMILES were also displayed.

    We will conduct comprehensive functional tests with the mechanically and electrically integrated HTV, such as conductivity verification of the pipes and electric system, and other compatibility tests. The HTV is then scheduled to be transported to the Tanegashima Space Center in April, 2009, at the earliest, and be launched by the H-IIB Launch Vehicle in the summer launch season of 2009 or later.

    Dec. 18, 2008 Updated
    All flight modules assembled for first time for inaugural HTV flight

    On Dec. 12, all the parts of the H-II Transfer Vehicle (HTV,) the supply transfer vehicle to the International Space Station, were assembled for an all-vehicle functional test ahead of its first flight. They are the “Logistic Carrier Pressurized Section,” the cargo section of the “Un-pressurized Carrier,” the “Exposed Pallet,” the “Avionics Module” and the “Propellant Module.” This was the first time that all the modules were assembled. The size of the assembled HTV was about the same size as the Pressurized Module of the Japanese Experiment Module “Kibo.” The HTV will be the largest payload that JAXA has ever launched.

    During the all-vehicle functional test, all the modules are mechanically and electrically connected to verify their function as one piece of the vehicle such as proper pipe routing and electric conductivity.

    The first HTV is scheduled to be launched by the H-IIB Launch Vehicle in September 2009 at the earliest.

    Aug. 28, 2008 Updated
    Thermal Vacuum Test for first flight of HTV

    A thermal vacuum test on the first flight vehicle of the H-II Transfer Vehicle (HTV) has been carried out at the Spacecraft Integration and Test Building at the Tsukuba Space Center.
    The purpose of the test is to evaluate the thermal design of the structure and to verify its endurance in the harsh environment of space by simulating the vacuum and thermal environment in space.
    Thermal vacuum tests for the Pressurized Carrier and Unpressurized Carrier have already been completed, and the main part with the Avionics Module and Propulsion Module combined is now in the 13-meter diameter space chamber for testing.
    The test will be completed in early September before the acoustic test and functional test are performed. After all the test results are reviewed to make sure that no problem is left unsolved, the vehicle will be transported to the Tanegashima Space Center for final launch preparations.

    (Photo: The main part of the HTV (Avionics Module and Propulsion Module) moved into the 13-meter diameter space chamber)

    Apr. 18, 2008 Updated
    The first model HTV (Technology Demonstration Model) was shown to the press

    On April 17, 2008, a press review was held for the first model H-II Transfer Vehicle (HTV) (Technology Demonstration Model), which is an unmanned cargo transfer spacecraft to the International Space Station. On display separately were the Pressurized Logistics Carrier for supply transportation, the Avionics Module for vehicle body control and the Propulsion Module which carries the propulsion system. When the HTV is completed and fully equipped, it will be the largest spacecraft in Japan with a length of 10 meters and a weight of 16.5 tons. After going through performance tests like the Thermal Vacuum Test and Acoustic Test, the first model HTV is scheduled for launch from Tanegashima on the H-IIB Launch Vehicle No. 1 (Test Model) in the summer of 2009.

    Jul. 2, 2007 Updated
    Proximity Communication System (PROX) undergoes testing

    Tests are currently being performed on the Proximity Communication System (PROX) at NASA’s Kennedy Space Center (KSC).

    The PROX system will be installed in the Japanese Experiment Module “Kibo” to communicate between the H-II Transfer Vehicle (HTV) and transmit and receive data between the International Space Station (ISS). It will also measure the relative distance and speed between the ISS and the HTV in order to support the HTV’s rendezvous with the ISS.

    Since last year, tests on the PROX and a compatibility test for the PROX/rack had been carried out before it went through a pre-shipping examination and was shipped out to the U.S. in January 2007. After performing several tests like the JEM/PROX compatibility test, it will be installed in the Experiment Logistics Module Pressurized Section (ELM-PS) and is scheduled for launch on Assembly Flight 1J/A at the end of February 2008.

    Photo1 : A general view of the PROX (Bottom right is the PROX before shipping at Tsukuba Space Center).
    Photo2 : A scene from a test on the PROX at the Kennedy Space Center.
    Photo3 : A crew review scene performed by astronaut Furukawa (taken from behind the PROX rack.)

    Jun. 26, 2006 Updated
    Prototype HTV unveiled to press at Tsukuba Space Center

    On June 23, a prototype of the H-II Transfer Vehicle (HTV) was unveiled to the press at the Tsukuba Space Center (TKSC.) The HTV is an unmanned orbital carrier to the International Space Station (ISS.) It is equipped with both the function of a “manned cargo carrier” for ISS crews to actually embark and carry out supportive work on it and the function of an “inter-orbital carrier” to perform “inter-orbit transportation to a selected attitude,” “rendezvous flights to the ISS,” and “re-entry” to aim to acquire the necessary technology for autonomous activities in space.

    The prototype will be used for various environment tests to make sure it can bear the extreme temperatures in space and acoustic and vibration environment at the time of launch. Through the tests, the project team will verify basic design data, and incorporate test results into future development.

    Outline of the HTV project

    Length about 10 m (including thruster)
    Diameter about 4.4 m
    Mass about 10.5 ton (excluding cargo)
    Loading capacity (for supply) about 6 tons
    Loading capacity (for waste) about 6 tons
    • Target orbit: ISS orbit
      Altitude: 350 to 460 km
      Inclination: about 51.6 degrees
    • Mission hours
      Solo flight: about 100 hours
      Stand-by: more than a week
      Docked with the ISS: about 30 days

    May 28, 2004 Updated
    Debris protection function was verified by shooting aluminum balls at the HTV at 6 km per second.

    Each module of the Space Station including the Japan Experiment Module has a “debris bumper” for protecting itself from losing its functions by colliding with space debris.
    The level of protection depends on the location (position) of each module and the probability of collision. Many technological ideas are incorporated to achieve the required protection effect, such as making the distance between the debris bumper and the pressurized wall longer.
    Solar array panels around the HTV have been considered to be part of the protective walls, but they needed to be verified.
    The verification was performed by a high-speed collision test using a HTV mockup. Aluminum balls of various sizes were shot at the protective walls at a speed of 6 km per second. After the test, the pressurized wall behind the protective walls was checked for holes. As a result, the solar array panels and the panel structure (an aluminum honeycomb structure) were verified to be effective for protection, and necessary data were also acquired for the further debris protection design assessment for the HTV.

    Upper Photo: A mockup for the verification (The thick wall on the right is a solar array panel.)
    Lower Photo:A solar panel from the back after the verification.

    Upper Photo: A mockup for the verification (The thick wall on the right is a solar array panel.)/Lower Photo:A solar panel from the back after the verification.;

    Mar. 28, 2003 Updated
    Manufacturing “Thermal Structural Test Models ” for Tests in the Next Fiscal Year

    HTV is about four meters in diameter and a bit shorter than 10 meters in length. In other words, its size can be explained as a container that could accommodate a sightseeing bus. In the process of developing HTV, therefore, it is divided into four modules namely Logistic Carrier Pressurized section, Logistic Carrier Un-Pressurized section, Avionics module, and Propulsion module. Thermal structural test models are being manufactured for each module. A thermal structural test model is a mimic model to test it in simulated harsh launch and space environments for checking acoustic condition, vibration, shock at separation and endurance in the space.

    The main structure is in conical semi-monocoque structure based on a launch vehicle design, and four modules will be assembled at the final fabrication phase and be tested for evaluating comprehensive strength and stiffness.

    Furthermore, tests for evaluating strength, pressure, acoustic data, shock, and heat balance, and acquisition of resonance frequency will be carried out to collect data for specifying environmental conditions of onboard loads and to find environmental characteristics data. The series of these tests will start in the next fiscal year.

    Upper Photo: Structural Thermal Test Model for Main Structure
    Lower Photo: Thermal Structural Test Model for Propulsion System “Helium Gas Supply Sub-Module”

    Oct. 5, 2001 Updated

    After HTV’s arrival to International Space Station (ISS), Exposed Pallet is taken out of HTV, and cargoes are replaced by robotic arm. This Exposed Pallet has rollers on its sides to minimize the friction and to keep the position accurately when it is brought back to HTV.
    A series of roller rotation slip tests was conducted from August to September 2001. The rollers are made of plastic to reduce the weight and they have solid lubricant on their surfaces. This combination of plastic and solid lubricant is rare. The purpose of this test is to confirm the manufacturing process and to collect the basic data of friction in the various environments (hot, cold, vacuum, air) and the wearing life.
    In addition, by conducting the test with the full-size model, the friction data closer to the actual operation were collected. The data will be applied not only for the HTV design and robotics analysis but also the future satellite programs and space equipment.

    Upper Photo: Setup for the rotation test in vacuum heat chamber
    Lower Photo: Setup for the full-size roller test

    Jun. 29, 2001 Updated

    Post Development Review of HTV Pressurized Carrier Aft Dome
    NASDA conducted additional preliminary design review (delta-PDR) with lots of participant from NASA and CSA (including ISS program manager) at Tsukuba Space Center as following schedule.
    Pre-Board Meeting : May 15th and 16th, 2001
    Board Meeting : May 18th, 2001
    We focused on two kinds of items in this review panel. One was a kind of additional items which were not reviewed in PDR held in 1999 (e.g.Un-pressurized carrier / Exposed pallet, GPS receivers in JEM, Crew operation panel, etc.) and another was a kind of items which had been changed the design from PDR (e.g. Solar power generation system, Approaching trajectory, etc.).
    Prior to holding the review panel, NASDA delivered review documents toward NASA, CSA and ESA and received a thousand of “Review Item Disposition Sheets (RID)” on these documents. We determined all dispositions for these RIDs after the discussions within three weeks. NASDA/NASA/CSA founded a few issues related to the ISS safety in this review panel and we determined to give high priority to these issues.

    Photo: HTV Delta-PDR Pre-Board Panel

    Feb. 19, 2001 Updated

    Post Development Review of HTV Pressurized Carrier Aft Dome A pressurized carrier equipped in HTV was designed based on the JEM Experiment Logistics Module Pressurized Section (ELM-PS). NASDA determined to use a newly designed integral molded structure for the Aft Dome of pressurized carrier to reduce the weight of 260 kg and the similar structure has already been used by the propellant tanks of Launch vehicles. Similar to H-IIA rocket, MAN-Technologie in Germany took the charge of the development under the supervision of Mitsubishi Heavy Industries LTD. Through this development, MAN-Technologie cleared the manufacturing problems such as thickness, welding, strength, etc., and completed them successfully. The photo shows a manufacturing sample that will be used for following engineering tests in Japan. After this review, NASDA will start manufacturing of the Flight Model and mass production.

    Photo: Aft Dome Structure for HTV Pressurized Carrier Engineering Test

    Dec. 8, 2000 Updated

    Succeeding to the previous tests conducted from April 18 to 20, 2000, NASDA/NASA/CSA conducted a series of real-time HTV capturing operation tests with expanded SSRMS conditions, evaluators, and facility by following schedule.
    Date: Nov. 8th to Nov. 10th, 2000
    Place: Canadian Space Agency Headquarter in Saint-Hubert, Quebec, CANADA
    In this series of tests, Astronaut Doi and other four astronauts executed total of up to 120 simulation- run cases with MOTS (MSS Operations and Training Simulator) in CSA, the facility with more complicated and numerous equipments. Just like previous tests, Astronauts evaluated the operability, by controlling SSRMS and executing capturing operation with free drifting HTV within predefined time. Though the results are still under investigation, the operation time was improved by re-designed operation sequence based on the experience in last tests.
    Photo (Upper): Astronaut Doi trying to capture Photo (Lower): CSA members supporting

    Nov. 9, 2000 Updated

    When crew enters HTV pressurized carrier berthed to ISS, it is necessary to circulate atmosphere in pressured cabin. The fan system for air circulation should meet several requirements such as large flow rate, low noise, lightweight, compact size, and high durability for severe environment during launch. Because each HTV mission period is relatively short, NASDA plans to develop a new air circulation fan system that is appropriate to HTV requirements.
    NASDA is conducting a series of development tests with this new fan system in Shinko-Denki Co. The purpose of tests is to ensure the silent and low vibration design with multi-stage/coaxial concept and new blade/housing shape. NASDA will then review the test results and reflect them to the final fan design.

    Photo: Test Setup

    Oct. 6, 2000 Updated

    The Pre-Shipping Review (PSR) for 28 R-1E thrusters, that will be used for HTV attitude control was held by Primex Space Systems Co. in the United States. These thrusters will be delivered to Ishikawajima-Harima Heavy Industries Co. Then after used in System Firing Test (SFT) in which NASDA confirms the Propulsion-system performance, they will be installed to the first HTV.
    The same thrusters have been used in Space Shuttle for attitude control and they will be installed in Propulsion Module of International Space Station.

    Photo: 28 sets of R-1E thruster (Offered by Primex Space Systems Co.)

    Jul. 7, 2000 Updated

    HTV has two carrier sections, one is a pressurized section which carries the logistics to ISS pressurized section and another is an un-pressurized section which carries experiment devices in ISS exposed section. The exposed experiment devices will be taken out from un-pressurized section with exposed pallet by ISS manipulator (SSRMS).
    From April 10 to June 8, NASDA had conducted Breadboard test in Mizuho facility of Ishikawajima-Harima Heavy Industries Ltd. for Paraffin Actuator that will be used for separation mechanism between exposed pallet and experiment devices. The Paraffin Actuator drives the output pin using phenomena of increasing of volume when paraffin changes its phases from solid to liquid and this attracts attention as a shock-less separation mechanism. In this series of tests, NASDA conducted a nominal driving test, environmental (vacuum/high temperature/low temperature) driving tests and a data-gathering test. NASDA obtained several data and the results will be used to improve the design of HCAM (HTV Cargo Attachment Mechanism).

    May 26, 2000 Updated

    HTV will perform autonomous rendezvous flight to the ISS, however, in the final operation, HTV will be captured by ISS manipulator system (SSRMS) controlled by ISS crew and be berthed to the ISS. Such operation is a peculiar requirement for HTV and we must confirm that it can be certainly captured by ISS crew within the limited time.
    To investigate the feasibility of this operation, a series of SSRMS capturing simulation test was conducted at MD-R (MacDonald Dettwiler Space and Advanced Robotics Limited) in Brampton City, Ontario, Canada from April 18 through 20. Besides four astronauts including Mr. Takao Doi, engineers from NASDA, CSA, and NASA had joined this test.
    In this simulation test, astronauts evaluated by controlling SSRMS and executing capturing operation in computer simulator: MDSF-RT (Manipulator Development and Simulation Facility in Real-Time) which HTV dynamics data from NASDA had been already input. Though details of the result are still under investigation, astronauts judged that this operation is feasible difficulty and it seemed that there are not any critical issues.

    Photo: HTV Capture Real-Time Crew Evaluation (offered by MD-R)

    Apr. 21, 2000 Updated

    In this month, NASA held the following safety review panel toconfirm the HTV safeness regarding to the International Space Station.
    HTV Safety Review Panel (Phase 1): March 13th to March 17th at Johnson Space Center in Houston.
    NASA holds the Safety Review Panel to all segments that compose the ISS and all approaching vehicles in rendezvousing to the ISS. Especially, HTV, which is the first newly designed transfer vehicle, turned out to be reviewed first in this panel. In this review panel, NASA and NASDA members had an animated discussion focused not only upon the hardware safety for the transfer vehicles such as logistics carrier and propulsion system but also upon the safety of flight-plan for rendezvous to the ISS. As a result, NASA confirmed the feasible of the HTV safety design and approved NASDA to progress the next design phase.

    Photo: Safety Review Panel Members

    Jan. 31, 2000 Updated

    PDR (Preliminary Design Review) for SIGI (Space Integrated GPSR/IMU) which is most important sensor of HTV Guidance and Navigation System was conducted at Honeywell co. in Tampa, Florida in United States from Dec. 9 to 10.
    In addition to accelerometers and ring laser gyros for control of HTV attitude/maneuver, this sensor unifies GPS receiver for navigation into one package.
    SIGI is also used in International Space Station to measure the attitude, and H764, the base of SIGI, are used in many aircraft.

    Figure: HTV Guidance and Control Schematic

    Dec. 17, 1999 Updated

    PDR (Preliminary Design Review) for Rendezvous Sensor which to be used during the HTV final approach was conducted at Daimler Chrysler Jena-Optronik in Jena, Germany from Nov.15 to 18. This sensor will also be used for ATV(Autonomous Transfer Vehicle) being developed by ESA.
    We expect a cost reduction / risk decrease become possible by this joint supply of NASDA-ESA.

    The figure: rendezous sensor function during final approach

    Nov. 19, 1999 Updated

    NASDA conducted the Approach/Release (Rendezvous) Flight Technology Test on the ETS-VII, which has close relation to the HTV rendezvous technology from Oct. 26 to 27.
    During the test, ETS-VII tried the R-bar approach which simulates the HTV final approach trajectory to the ISS. HIKOBOSHI satellite regarded as HTV, approached to the virtual R-bar formed by ORIHIME, using the algorithm developed for HTV. As a result, HIKOBOSHI raised the appropriate orbit within the expected corridor determined for rendezvous sensor and successfully finished at the 114 meters close.
    We are now analyzing the data obtained from this experiment. It will greatly contribute to the establishment of all HTV flight algorithm.

    Sep. 17, 1999 Updated

    NASDA held two major review meetings. One was the HTV Phase 1 Safety Review, which examined the HTV design from the point of safety. The another was HTV Preliminary Design Review (PDR), which examined the HTV design from the point of technique.
    The safety review meeting was held from August 18 to 20. The safety design of HTV was generally confirmed. After some additional study, HTV project will take a NASA safety review.
    The HTV PDR meeting was held by NASDA from August 23 to September 3. Approximately forty NASA, European Space Agency (ESA), and Canadian Space Agency (CSA) people attended the meeting and examined the HTV design. As the result of review, design of HTV was confirmed to be adequate. Therefore, the production of HTV Engineering Model (EM) and the progress to detailed design phase were admitted.

    Jul. 26, 1999 Updated

    The documents for PDR (Preliminary Design Review), which will be conducted from July 15th to September 3rd have been released. These documents have also been sent to NASA, CSA, and ESA in the end of June.
    We will continue to coordinate with reviewers of both NASDA and other organizations on matters which they point out until PDR Main Board.
    At the same time, the documents for Phase 1 Safety Review have been released.

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  • [Institute of Space and Astronautical Science (ISAS)] The Forefront of Space Science: Honeycomb-structured Weight-saving High Gain Planar Antennas Installed on Hayabusa 2

    TOP > Report & Column > The Forefront of Space Science > 2014 > Honeycomb-structured Weight-saving High Gain Planar Antennas Installed on Hayabusa 2

    The Forefront of Space Science

    Honeycomb-structured Weight-saving High Gain Planar Antennas Installed on Hayabusa 2

    | 1 | 2 | 3 |

    The asteroid explorer “Hayabusa 2” was launched on 3 December. This paper will introduce the high gain planar antennas lightened with the use of honeycomb structure which is hexagonal just like a honey comb. Additionally, we will also talk about the synthetic aperture radar system for small satellites which is currently under development with the same honeycomb structure.

    High Gain Planar Antennas Installed on Hayabusa 2

    Figure 1 shows the illustration of Hayabusa 2. The two disk-shaped objects installed on the upside of its body are the high gain planar antennas. One is the X-Band (8.4GHz) antenna which is also installed on the Venus Climate Orbiter “AKATSUKI” launched in May 2010. Another one is the Ka-band (32.0GHz) antenna. To make the gain of the antennas higher and increase transmission speed, the Ka-band which is of higher frequency and the X-Band which is adopted in many earth stations are used as a combination.

    Diameters of both antennas are around 90cm, but about 1kg of weight was saved with the use of honeycomb structure in waveguides for radio waves.

    Figure 1
    Figure 1. The asteroid explorer “Hayabusa 2”
    Of the two circular plate installed on the upper surface of the explorer body, the left is the Ka-band(32.0GHz) antenna and the right is the X-Band(8.4GHz) antenna.
    | 1 | 2 | 3 |

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  • [Project Topics] Development progress for Enhanced Epsilon

    Topics List

    Aug. 6, 2015 Updated
    Development progress for Enhanced Epsilon

    The development of the Enhanced Epsilon Launch Vehicle has been going smoothly.
    The static firing test of the sub-sized upper-stage motor was completed before the end of March, 2015, as scheduled.
    On June 18, shocks and behavior due to the payload separation impact were checked through the pyro-shock test at the Sagamihara Campus.
    The Enhanced Epsilon has a better launch capacity compared to the first Epsilon launched in Sept. 2013. The goal is to launch the Exploration of energization and Radiation in Geospace “ERG” in JFY 2016.

    Development progress for Enhanced Epsilon

    Nov. 7, 2013 Updated
    Epsilon Launch Vehicle awarded Good Design Award Gold Award

    The first Epsilon Launch vehicle (Epsilon-1) developed and launched by JAXA in September 2013 received the JFY 2013 Good Design Award Gold Award sponsored by the Japan Institute of Design Promotion.
    Epsilon was listed as one of the 1,212 Good Design Award winners from 3,400 nominees, then selected for the best 100 products, and finally chosen for the Gold Award this time.

    Epsilon Launch Vehicle awarded Good Design Award Gold Award

    Sep. 14, 2013 Updated
    Launch Result of Epsilon-1 with SPRINT-A aboard

    JAXA launched the first Epsilon Launch Vehicle (Epsilon-1) with the Spectroscopic Planet Observatory for Recognition of Interaction of Atmosphere (SPRINT-A) onboard at 14:00 on September 14 (Sat.), 2013 (Japan Standard Time, JST) from the Uchinouora Space Center.
    The launch vehicle flew smoothly, and, at about 61 minutes and 39 seconds after liftoff, the separation of the SPRINT-A was confirmed.
    We would like to express our profound appreciation for the cooperation and support of all related personnel and organizations that helped contribute to the launch of the Epsilon-1.
    The satellite is currently in good health.
    The SPRINT-A’s nickname was also decided. It is “HISAKI”.

    Sep. 12, 2013 Updated
    Epsilon-1/SPRINT-A new launch date decided!

    JAXA would like to announce that we have set the launch date and time of the first Epsilon Launch Vehicle (Epsilon-1) with the Spectroscopic Planet Observatory for Recognition of Interaction of Atmosphere (SPRINT-A) onboard as follows.

    Scheduled launch day: September 14 (Saturday), 2013
    Scheduled launch time: 1:45:00 p.m.

    JAXA will broadcast a live launch report from the Uchinoura Space Center from 1:25 p.m. on the day. You can watch it through the Internet.
    Please send your support message for the launch on the special website, or tweet it including #Epsilon JAXA.

    Sep. 9, 2013 Updated
    New Launch Day Information for Epsilon-1 with SPRINT-A Onboard

    The Japan Aerospace Exploration Agency (JAXA) decided to postpone the launch of the first Epsilon Launch Vehicle (Epsilon-1) with the Spectroscopic Planet Observatory for Recognition of Interaction of Atmosphere (SPRINT-A) onboard on August 27 from the Uchinoura Space Center. As a result of our cause investigation of the postponement and re-examination of the Epsilon-1, the new launch date will be September 14, 2013 (Japan Standard Time) or later.

    Aug. 28, 2013 Updated
    Updated Information about Epsilon-1 Launch Day

    The Japan Aerospace Exploration Agency is now investigating the cause of an automatic stop alarm issued approximately 19 seconds prior to liftoff during the Epsilon-1 launch countdown operation on August 27, 2013. As we have decided to carefully examine the cause and prudently confirm the measures, it is very difficult for us to set the new launch date within August.
    We will inform you about the results of our investigation into the cause and the new launch date as soon as they are respectively clarified.
    Thank you for your patience.

    Aug. 27, 2013 Updated
    Launch Cancellation of Epsilon-1 with SPRINT-A Onboard

    The Japan Aerospace Exploration Agency (JAXA) cancelled today’s launch of the first Epsilon Launch Vehicle (Epsilon-1) with the Spectroscopic Planet Observatory for Recognition of Interaction of Atmosphere (SPRINT-A) onboard from the Uchinoura Space Center, because an automatic stop alarm was issued as an attitude abnormality was detected approximately 19 seconds prior to the liftoff time during the automatic countdown sequence. The launch had been originally scheduled for 1:45:00 p.m. today (Japan Standard Time).
    JAXA is currently investigating the cause.

    Aug. 8, 2013 Updated
    Launch Postponement and Launch Time Change for Epsilon Launch Vehicle with SPRINT-A onboard

    The Japan Aerospace Exploration Agency (JAXA) decided to postpone the launch of the first Epsilon Launch Vehicle (Epsilon-1) with the Spectroscopic Planet Observatory for Recognition of Interaction of Atmosphere (SPRINT-A) onboard to August 27, 2013,?from the Uchinoura Space Center as JAXA has taken extra time to rectify the incompatibility* found in the ground support equipment during the communication function test between the Epsilon-1 and the equipment in the course of launch campaign at the launch site. The launch was originally scheduled for August 22, 2013 from the center.

    Scheduled launch day: August 27 (Tue.) 2013
    Scheduled launch time window: 1:45 thru 2:30 p.m.

    Jun. 17, 2013 Updated
    Epsilon Support Message Campaign result!

    The Message Campaign for the first Epsilon launch vehicle scheduled to be launched on Aug. 22 was held in April and May, and the result of the campaign is now available on our website.
    You can check if your message was selected by your receipt number. Many people, more than expected, participated in the campaign. Thank you very much. Please also confirm where your message is loaded through the page.

    May 21, 2013 Updated
    Spectroscopic Planet Observatory for Recognition of Interaction of Atmosphere (SPRINT-A) launch by Epsilon-1

    The first Epsilon Launch Vehicle (Epsilon-1) with the Spectroscopic Planet Observatory for Recognition of Interaction of Atmosphere (SPRINT-A) onboard is determined to be launched on August 22 (Thursday, Japan Standard Time). The launch time is between 1:30 thru 2:30 p.m. (JST), and the launch site is the Uchinoura Space Center.
    Also, the design of the Epsilon 1 was decided! It expresses the tradition and future of the solid-fuel launch vehicle. We are now incorporating your messages in to the design. They were collected through the “Epsilon-1 support message campaign”, which ended on May 7. We received 5,812 messages in total. Thank you very much for your participation.

    Apr. 10, 2013 Updated
    Epsilon Message Campaign

    The Japan Aerospace Exploration Agency (JAXA) will launch the first Epsilon Launch Vehicle (Epsilon-1) in the 2013 summer launch season from the Uchinoura Space Center in Kimotsuki, Kagoshima Prefecture, with the spectrographic planet observation satellite (SPRINT-A) onboard.
    JAXA would like to hold a message campaign to welcome your messages on your expectations, hopes, dreams or feelings toward our new launch vehicle, then post them on the vehicle as part of its design by processing them in strings of small letters. This is the first attempt in Japan to place messages on the launch vehicle design.
    Through this campaign we hope that you can deepen your understanding of our next generation solid-fuel launch vehicle Epsilon and feel closer to it, so that we can “make people feel more familiar with space, gaining more understanding of and support for space programs.” This is one of the goals of the Epsilon project. Please join our campaigns!

    Oct. 15, 2012 Updated
    Extension test of the second stage motor nozzle

    The extension test of the second stage motor nozzle of the Epsilon Launch Vehicle was held at the Sagamihara Campus in late September.
    This extension nozzle is a technology that was adopted for the kick motor of the M-3SII Rocket launched in 1989. The nozzle is extended by the force of a light-weighted spring shortened and installed inside the nozzle.
    The test this time checked the spring and extension mechanism of the nozzle for M-34c, the renovated type from the nozzle for the third stage motor M34b of the M-V Launch Vehicle. The nozzle was verified to work properly through the test.

    Jul. 18, 2012 Updated
    PBS pyro-shock test

    Loaded with a small liquid-fuel engine, the Post Boost Stage (PBS) will be additionally installed on the top of the third stage when higher orbit insertion accuracy is required. The pyro-shock test of the PBS was performed at the Sagamihara Campus in mid June.
    The PBS is expected to be used more in low-orbit missions, and it enables the launch vehicle to place a payload more precisely in its scheduled orbit.
    The test this time was to verify if the PBS was strong enough to bear with the separation shock from the launch vehicle. A tremendous shock occurs at the time of separation, thus the shock levels for each part were measured. We have confirmed that no problem was found in the PBS through the test.

    Apr. 17, 2012 Updated
    Epsilon: acoustic environment measurement test at mockup launch pad

    JAXA made a mockup launch pad on a scale of 1/42 in order to confirm the acoustic environment according to the launch pad configuration. The mockup was based on the design analysis performed mainly by the Epsilon Launch Vehicle Project Team. The acoustic environment measurement test at the mockup launch pad by a small-scale solid motor has been held three times since April 2011 at the Noshiro Rocket Testing Center.
    The noise at the time of launch affects not only life in the surrounding area, but also the payload of a launch vehicle including onboard devices of a satellite. Therefore, it is one of the decisive factors for launch. The larger the expected vibrations cause by the launch noise, the greater the margin is required for vibration proof design.
    By understanding the acoustic characteristics of launch at the designing stage of the launch site, and taking appropriate measures, we can improve the launch environment for higher reliability, reduce costs and make the site more user-friendly so that the Epsilon’s competitiveness is enhanced.
    Through the three test series including the one this time, we were able to acquire very useful data that satisfies our purposes as we found the launch pad configuration can mitigate its acoustic environment.

    Sep. 30, 2011 Updated
    Static firing test for the upper stage sub-size motor

    On September 30, JAXA performed the ground firing test of the sub-size motor (M-34SIM-3) for the Epsilon Launch Vehicle upper stage at the Noshiro Rocket Testing Center. The test mainly aims to verify the insulation material on the upper motor nozzle that is currently under development.
    Through this test, we are steadily progressing with the Epsilon development while confirming the insulation function of the upper motor nozzle part based on the test results and maintaining and inheriting the already acquired solid motor static firing test technology.

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  • [Project Topics] AKATSUKI: Orbit successfully controlled

    Aug. 5, 2015 Updated

    AKATSUKI: Orbit successfully controlled

    AKATSUKI: Orbit successfully controlled

    JAXA performed an orbit control maneuver for the Venus Climate Orbiter “AKATSUKI” in late July in preparation for its re-injection into the Venus orbit scheduled for Dec. 7, 2015. According to the analysis of telemetry data acquired up to Aug. 2, the orbit control and correction was successfully conducted as scheduled by 5:30 p.m. on August 4. (All dates and time are Japan Standard Time.) …

    About Venus Climate Orbiter “AKATSUKI” (PLANET-C)

    (Courtesy of Akihiro Ikeshita)

    AKASTUKI will elucidate the mysteries of Venus, Earth’s twin sister.
    Japan will initiate the beginning of a new era of Venusian exploration.

    AKATSUKI (PLANET-C) is the next planetary exploration project for the Martian orbiter NOZOMI. Venus has long been referred to as Earth’s sister planet not only because its size and distance from the sun are similar to those of the Earth, but also because its birth formation is considered to be similar to that of the Earth at the genesis period of the solar system. However, Venus is actually very different from the Earth as it is veiled in high-temperature carbon dioxide and thick sulfuric-acid clouds. Also, above the surface of Venus, violent winds which reach some 400 kilometers per hour blow over. Clarification of the causes for such an environment will provide us with clues to understand why the Earth has become a peaceful and lively planet unlike Venus as well as to help understand climate change on Earth. Therefore, Venus is a very important subject for exploration to learn about the Earth’s environment.

    Launch date: May 21, 2010

    Re-entry plan to Venus orbit

    The AKATSUKI is expected to usher in a new era of Venusian exploration. It was launched aboard an H-IIA Launch Vehicle No. 17 in May 2010 (JST.) It smoothly flew and spurted out jets from its orbit control engine on Dec. 7, 2010. Unfortunately, the AKATSUKI failed to inject itself into the orbit of Venus. JAXA set up an investigation team not only to examine and study the causes of the failure and countermeasures, but also to see if it is possible to insert the AKATSUKI again into the orbit when it comes closer to Venus in about six years.

    Characteristics of Venus Climate Orbiter “AKATSUK” (PLANET-C)

    Infrared light enables more detailed investigation of Venus.

    The probe vehicle of AKATSUKI will enter an elliptical orbit, 300 to 80,000 km away from Venus’s surface. This wide variation in distance will enable comprehensive observations of the planet’s meteorological phenomena and of its surface, as well as observations of the atmospheric particles escaping from Venus into space. It will also be possible to take close-up photos of Venus, and to observe the storm winds that blow on the Venusian surface, at speeds that reach 100 m a second – 60 times the speed at which Venus rotates. This phenomenon remains the biggest mystery of Venus, as it cannot be explained meteorologically. AKATSUKI will employ infrared light to observe and elucidate the mysteries surrounding the atmosphere under the clouds and the conditions on the planet’s surface. In addition, it will confirm the presence of active volcanoes and thunder.

    Major Characteristics

    International Designation Code 2010-020D
    Launch Date 6:58, May 21, 2010 (JST)
    Launch Vehicle H-IIA Launch Vehicle No.17
    Location Tanegashima Space Center
    Shape Box shape with two wing-type solar array paddles
    Weight Mass at liftoff: about 500 kg
    Orbiter Venus elliptical orbit
    Altitude PeriVenus: 300 km
    ApoVenus: about 80,000 km
    Orbital Inclination Approx. 172 degrees
    Orbital Period Approx. 30 hours

    Mission talk by team leaders

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  • [Aeronautical Technology Directorate] [DREAMS] JAXA has conducted a usability survey of the "ALWIN" at Tokyo International Airport

    June 30, 2015

    JAXA has conducted a usability survey of the “ALWIN” at Tokyo International Airport

    JAXA has conducted a usability survey of the “Airport Low-level Wind INformation” (ALWIN) for airline’s flight crews and dispatchers in cooperation with Japan Airlines (JAL) at Tokyo International Airport (Haneda Airport) on March 2015.
    ALWIN provides strategic aircraft operational information on low-level wind which includes turbulence and windshear in the vicinity of the airport using an airport Doppler lidar. The wind information generation logic and display prototype of ALWIN has been jointly developed by JMA (the Japan Meteorological Agency) and JAXA.
    Flight crews are able to obtain ALWIN at any time on request by using an automatic ACARS (Aircraft Communications Addressing and Reporting System) *1 text uplink by using the ACARS text conversion function of ALWIN and data link server. On the other hand, dispatchers/airport-based operations officer are able to acquire graphical displays of ALWIN by internet web page.
    The airline usability survey results will reflect design specifications of ALWIN when integrating ALWIN to MetAir (JMA’s aviation weather information web page) in the future.

    Flight crew’s usability survey of ALWIN:


    The photograph on the left shows JAL’s Office of Haneda Airport.
    In the office, flight crews confirm weather conditions required for aircraft operational planning.
    To survey how flight crews use ALWIN in actual aircraft operation, a JAXA research engineer joined JAL’s flight crews during regularly scheduled flight from a preflight briefing to debriefing.

    Flight crews are able to check wind conditions on the flight by ALWIN web screen in preparation of take-off from Haneda airport. When there is severity information related to windshears or strong gusts exist on the flight path, the altitude band of the significant wind change is highlighted in amber color in headwind and crosswind graph of the ALWIN screen to enable intuitive understanding of the alert information. The ALWIN also can be utilized to briefing before takeoff.

    In this flight crew’s usability survey, a JAXA research engineer carried out cockpit observation from on the jump seat of the Boeing 777 in domestic flights: Haneda-Chitose, Chitose-Haneda.

    During cockpit preparation before takeoff, the copilot clicks the function key for ACARS uplinks relating to ALWIN on the MFD (Multi-Function Display) by mouse to confirm wind condition of ALWIN.

    Cruise phase from Chitose to Haneda:
    Before the descent, the flight crew requests ALWIN-ACARS uplink to confirm wind conditions at Haneda Airport. Generally speaking, aircraft control for the approach / landing phase is said to be the most difficult for a pilot out of all aircraft controls. Especially when there is rapidly changing and low-level turbulence on a landing path, difficulty of aircraft control for landing increases. Such wind conditions occurring at low altitudes during takeoff or landing can lead to the risk of serious accidents. The frequent occurrence of the low-altitude turbulence known as a “hangar wave” *2 at Haneda Airport led to request for implementation of ALWIN at the airport.

    Close-up view of ALWIN:
    ACARS is not capable of sending graphical information to the cockpit, but is capable of sending the text messages. During the high workload approach flight phase, the flight crew’s intuitive understanding is highly important because a rapid but accurate situation assessment of wind disturbances is required. Considering this situation, JAXA has designed an ACARS message containing a spatial graph rendered as test as shown in the upper picture. The spatial graph shows headwind profile on the landing path below 500 ft in the ACARS message texts. Moreover, the message texts contain the headwind component, wind direction / speed and crosswind component per altitude.

    ALWIN printout:
    Although the flight crew is required to scroll the screen to see both headwind profile and crosswind profile on the MFD, the ALWIN printout enables flight crews to confirm headwind profile (upper) and crosswind profile (lower graph) on one page of paper. Essential wind information for approach/landing planning was selected due to layout limitation, because the number of characters which can be sent using ACARS is limited.

    The PM (Pilot Monitoring) explains wind situations by the ALWIN ACARS text message. Based on this information, the PF (Pilot Flying) makes approach/landing planning.
    The approach briefing by using ALWIN provides flight crews with common situational awareness relating to approach/landing planning which takes into accounts wind conditions.

    We are approaching to the Runway 23 (runway bearing of 230 degrees) at Haneda Airport for arrival.


    After landing, the JAXA research engineer conducted an interview with flight crews regarding the usability of ALWIN. Flight crews commented that ALWIN was helpful because it gave flight crews an intuitive understanding of no significant wind change below 500ft and common situational awareness during approach briefing.
    After returning to the Office, flight crews wrote questionnaire sheets prepared by JAXA. Although little severe wind conditions had been experienced on the today’s flights, flight crews indicated on the questionnaire that the ALWIN ACARS text message was useful. The reason for usefulness was stated as follows: “We could confirm in advance that no significant difference existed between wind conditions during the final approach and those on the ground.”

    We could obtain feedback from only a few flight crews by interviews. However, by using the survey in questionnaire format in writing, we will collect a large number of opinions on the usability of ALWIN from many flight crews. Therefore, the airline usability survey results will reflect future improvement of ALWIN design specifications for ALWIN implementation in cooperation with JMA.

    *Special permission was acquired for cockpit photography.

    Airline dispatcher’s usability survey of ALWIN:

    The JAL’s domestic and international flights are centrally controlled by the JAL Operation Control Center (JAL OCC) at Haneda Airport. JAXA research engineer observed how airline dispatchers use ALWIN at the JAL OCC.


    The desks of airline dispatchers are divided into international flights and domestic flights. ALWIN is one of the screens shown in the photograph on the left.

    The photo shows an example of past data display of ALWIN.
    For emphasizing the past data, the word “Past” is shown in large font at the top of the screen. This past data is from around 20:35 on March 1, 2015. The data shows a significant change in wind conditions at Haneda Airport (RJTT). The past data display is one of the favorable functions for airline’s users, because the users are able to utilize past data for flight critique or past wind conditions analysis.

    ALWIN can also present historical information for the previous several hours. The provision of history information is aimed to help to understand daily tendency of wind direction and speed, windshear and to accumulate knowledge for periodical wind situations.

    The JAXA research engineer conducted an interview with JAL’s dispatcher regarding the usability of ALWIN.
    Dispatchers commented that they use ALWIN to confirm current wind conditions and the altitude band of the significant wind change.

    At JAL, automatic ACARS uplink of ALWIN is possible at any time on the flight crew’s request. Therefore, there are almost no cases in which airline dispatchers check ALWIN and then advise to the cockpit by ACARS manual uplink or by radio communications. However, dispatchers indicated that ALWIN would be useful for understanding of wind conditions regardless of whether or not a go-around is anticipated.

    ※1: ACARS (Automatic Communications Addressing and Reporting System)
    A digital datalink system between aircraft and ground stations. Via the ARINC communication network, required flight information is automatically sent from aircraft to ground stations or from ground stations to aircraft.
    ※2: Hangar wave
    Refers to turbulence thought to occur when strong northeasterly or easterly winds pass over hangers located in the newly developed area on the southern side of Haneda Airport. The hangar wave affects aircraft taking off and landing at Runway A (34L) on the western side of the hangars.

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  • [Aeronautical Technology Directorate] [SafeAvio] Simulation for effect on passenger cabin when encountering turbulence

    July 13, 2015

    Simulation for effect on passenger cabin when encountering turbulence

    To determine turbulence effects on the passenger cabin, JAXA conducted simulations for the following two cases. Motion of aircraft, a cabin crew and service carts were simulated for both cases.

    The left-hand side of the video below simulates a case of severe turbulence when an aircraft experienced sudden change in altitude (maximum -0.7 G of vertical acceleration).

    The right-hand side, meanwhile, simulates a case where such vertical acceleration of aircraft is reduced by half with the gust alleviation technologies which we are developing under the SafeAvio initiative. The result shows that cutting turbulence shaking in half eliminates almost all risks of injury in the passenger cabin.

    This simulation data will be used in further research on gust alleviation technology, and for reviewing the operating procedures of cabin crews.

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  • [ISS / Japanese Experiment Module (KIBO)] Free-Space PADLES experiment conducted

    Free-Space PADLES experiment conducted

    Last Updated: July 14, 2015

    The first Free-Space PADLES experiment intended to investigate the space radiation dose outside the Japanese Experiment Module “Kibo” was conducted from June 1-15, 2015.

    PADLES will be shipped to the JAXA Tsukuba Space Center (TKSC) for analysis after its return to earth. During this technology demonstration mission, the following will be closely evaluated:

    • The space radiation environment in Low Earth Orbit (LEO)
    • The hull wall capability of Kibo as compared to its internal environment

    The results of this experiment using PADLES will provide basic data useful for the risk assessment of Extravehicular Activities (EVA), and the assessment and optimization of hull wall thickness for manned spacecraft.

    The next experiment is scheduled in March 2016 or later.

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    Astronaut Scott Kelly verifies the retrieved Free-Space PADLES (June 17, 2015) (Credit: JAXA/NASA)

    Retraction to Kibo’s airlock

    On June 15, under remote control from the TKSC, Kibo’s robotic arm with Free-Space PADLES attached to the Multi-Purpose Experiment Platform (MPEP) was transferred from the exposure point to in front of Kibo’s airlock door. PADLES on the MPEP was then retracted into the airlock.

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    MPEP being transferred to the airlock (June 15, Credit: JAXA/NASA)

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    The MPEP being transferred to the airlock on June 15 (Credit: JAXA/NASA)

    Free Space PADLES retraction [1 min., 54 s] (Credit: JAXA/NASA)

    Retrieval to the Kibo’s PM

    The MPEP was retracted into the Kibo’s airlock. After depressurization to 1 atm, Astronaut Scott Kelly retrieved PADLES for its return to earth.

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    Retracted MPEP (Credit: JAXA/NASA)

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    Free-Space PADLES being removed from the MPEP (Credit: JAXA/NASA)

    Digest video showing Free-Space PADLES retrieval [1 min., 28 s] (Credit: JAXA/NASA)

    Various types of experiments using PADLES have been conducted since 2008 with the launch of Kibo modules.

    See also:
    PADLES database
    Free-Space PADLES

    Responsible unit:
    JEM Mission Operations and Integration Center
    Human Spaceflight Technology Directorate
    JAXA Tsukuba Space Center

    *All times are Japan Standard Time (JST)

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  • [International Space Station / Japanese Experiment Module (KIBO)] JAXA Astronaut Activity Report, February 2015

    JAXA Astronaut Activity Report, February, 2015

    Last Updated: May 11, 2015

    This is JAXA’s Japanese astronaut activity report for February, 2015.

    Astronaut Kimiya Yui continues training for his upcoming long-duration ISS mission

    Astronaut Kimiya Yui, who was assigned as a crew member for the Expedition 44/45 mission to the International Space Station (ISS), underwent training for this long-duration mission at the NASA Johnson Space Center (JSC) at the beginning of February, followed by training at the GCTC for the rest of the month.

    At the JSC, training was held for Extravehicular Activity (EVA) and the Space Station Remote Manipulator System (SSRMS). During EVA training in the large pool in the Neutral Buoyancy Laboratory (NBL) where a mock-up of the H-II Transfer Vehicle (HTV) “KOUNOTORI” is submerged, Yui donned a submersible Extravehicular Mobility Unit (EMU) and dived into the water. Yui experienced a scenario where a payload loaded on the KOUNOTORI’s Exposed Pallet (EP) had to be removed by conducting unscheduled EVA.

    Using a Virtual Reality (VR) system, Yui and his crewmate Kjell Lindgren also trained together to master how an EVA member and a SSRMS operations member tie up to proceed with EVA tasks. During the training, Yui was in charge of SSRMS operations and confirmed the procedure for supporting the crew’s EVA operations.

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    Yui and his crewmates training in the Soyuz simulator (Photo courtesy of JAXA and the GCTC)

    The training in Russia was focused on flight simulation aboard the Soyuz spacecraft. Alongside Soyuz commander Oleg Kononenko and Astronaut Lindgren, Yui practiced each stage of operations ranging from launch and docking with the ISS, to returning to Earth after undocking from the ISS. They rehearsed operations in manual control mode that is used as backup in case automated control mode fails, as well as responses to sudden depressurization during a flight. For the ISS Russian segment, Yui’s training covered proper responses to such emergencies as an outbreak of fire and sudden depressurization.

    Astronaut Takuya Onishi undergoes survival training in Russia

    Astronaut Takuya Onishi, a crew member for the ISS Expedition 48/49 mission, underwent training at Russia’s Gagarin Cosmonaut Training Center (GCTC) during the first half of February, followed by training at the NASA Johnson Space Center (JSC) for the latter half of the month.

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    Survival training participants from left: Onishi, Rubins, and Ivanishin (Photo courtesy of JAXA and the GCTC)

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    Onishi making a fire (Photo courtesy of JAXA and the GCTC)

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    The trio setting up a shelter (Photo courtesy of JAXA and the GCTC)

    In Russia, Onishi participated in survival training under an assumed case of the Soyuz spacecraft being forced to make an emergency landing on a snow-covered mountain or in a snowfield. This on-site training is intended to help participants learn survival skills by cooperating with each other. Onishi spent outdoor life in sub-zero temperatures with two other participants: Russian Cosmonaut Anatoly Ivanishin and NASA Astronaut Kathleen Rubins, who will fly together with Onishi aboard the Soyuz spacecraft.

    The training was held for two nights and three days because two or three days may be required to conduct search and rescue operations in case the Soyuz spacecraft is forced to touch down at an unpredictable location. In the beginning, they changed from Sokol spacesuits to snowsuits aboard the Soyuz spacecraft. Then they selected a camping location and set up a shelter using the spacecraft’s parachute and hewn wood. The trio made a fire with the wood they collected, and then took turns tending the fire at night.

    The training included a simulated case of one crew member being injured. They practiced how to treat the injured crew member. They also ignited flares to signal a rescue team by following the specified procedure.

    In addition to undergoing survival training, the participants conducted simulated operations of the Soyuz spacecraft for the first time as a trio among all 46S crew members. Atmospheric reentry operations were also simulated under a hypergravity condition generated by a huge centrifuge accelerator, which recreated the gravity that Onishi would experience during this stage. For the Russian segment, Onishi confirmed the maintenance procedure of the Russian toilet as part of life support system training.

    At the JSC, Onishi was trained for overall ISS operations. In the ISS mock-up, Onishi and the other two crew members participated in an emergency response simulation that included cases of fire, sudden depressurization, and air contamination, and responded to each scenario in accordance with the specified procedures.

    Onishi also learned the duties of the Crew Medical Officer (CMO) to be performed in orbit, including medical-checkup and first-aid procedures.

    Onishi’s other training included capturing the H-II Transfer Vehicle (HTV) “KOUNOTORI” by using the Space Station Remote Manipulator System (SSRMS), engaging in simulated daily tasks according to a normal daily schedule on the ISS, and practicing image and video management onboard the ISS.

    Astronauts Soichi Noguchi and Akihiko Hoshide underwent flight piloting training

    Astronauts Soichi Noguchi and Akihiko Hoshide underwent about one week of flight training at Oita airport aboard the Hawker Beechcraft Baron G58 owned by Honda Airways.

    This training is intended to maintain and improve one’s multitasking ability–a qualification required of astronauts.

    Before the flight, Noguchi and Hoshide used a flight simulator to familiarize themselves with flying, and attended lectures on meteorology and flight plans. They also confirmed the procedure for preflight inspection and actually inspected the plane to be flown.

    During the flight training, Noguchi and Hoshide piloted the aircraft by only using the information shown on instrumentation to determine the aircraft’s attitude, height, position, and course, performed an aborted landing (go-around), and operated the aircraft in response to irregular conditions.

    Astronaut Satoshi Furukawa undergoes robotic arm training

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    During SSRMS operations training, Furukawa was joined by Wakata at the JSC (Credit: JAXA/NASA)

    Astronaut Satoshi Furukawa underwent robotic arm training from mid-January to February 6 at the NASA JSC, in order to refresh and further improve his skills.

    Using a robotic arm simulator, Furukawa performed SSRMS operations to support the EVA crew and capture unmanned supply vehicles such as KOUNOTORI. During this training, Astronaut Koichi Wakata–a leading expert on robotic arm operations–took the opportunity to join Furukawa and give him advice.

    JAXA astronauts participate in the opening event of Great Britain’s “Innovation is GREAT” campaign

    On February 27, the opening event of the “Innovation is GREAT” campaign organized by the British embassy was held in Roppongi, Tokyo. This yearlong campaign conducted by Japan and Great Britain is intended to promote their bilateral partnership, which includes fostering cooperation in the field of space development. His Royal Highness Prince William, Duke of Cambridge, who was visiting Japan at the time, delivered the opening remarks.

    For this campaign, Yui and British Astronaut Timothy Peake of the European Space Agency (ESA), who will stay on the ISS this year, each sent a video message.

    In his video message, Yui discussed that along with Peake, he wished that activities on the ISS would lead to innovation. Yui and Peake are fellow astronauts who were both selected as astronaut candidates in 2009, and have undergone the 16th NASA Extreme Environment Mission Operations (NEEMO) together. Following the commencement of Yui’s ISS stay in May, Peake will begin his ISS stay from November. In the video, Yui also gave several words of encouragement to Peake and mentioned that he would securely hand over the baton of ISS operations.

    Astronaut Soichi Noguchi had attended the event along with Prince William, and gave a Japanese traditional performance to celebrate the start of the campaign. During a talk session, they discussed the significance of the campaign. The event included a presentation given by British researchers and space industry representatives.

    Astronaut Chiaki Mukai receives the Legion of Honour

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    At the Ceremony: Mukai (left) and French Ambassador Thierry Dana (right)

    Astronaut Chiaki Mukai was conferred the National Order of the Legion of Honour (or Legion d’Honneur in French), Chevalier, from France. On February 3, French Ambassador Thierry Dana presented her with a decoration medal.

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