List of H-II series and H3 launches
Launch statistics
Launch sites
1
2
3
4
5
6
1994
1998
2002
2006
2010
2014
2018
2022
- Yoshinobu Launch Complex 1
- Yoshinobu Launch Complex 2
Launch outcomes
1
2
3
4
5
6
1994
1998
2002
2006
2010
2014
2018
2022
2026
- Success
- Partial failure
- Failure
- Planned
Launch history
1994-1999 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
---|---|---|---|---|---|---|---|---|
TF1 (Test Flight) | February 3, 1994 22:20 |
H-II | LA-Y1, Tanegashima | OREX (Orbital Re-entry Experiment), VEP (Vehicle Evaluation Payload) | LEO / GTO | Success | ||
Ryūsei, Myōjō | ||||||||
TF2 | August 28, 1994 07:50 |
H-II | LA-Y1, Tanegashima | ETS-VI (Engineering Test Satellite-VI) | GEO | Success | ||
Kiku 6 | ||||||||
TF3 | March 18, 1995 08:01 |
H-II | LA-Y1, Tanegashima | GMS-5 (Geostationary Meteorological Satellite-5) / SFU (Space Flyer Unit) | GEO / LEO | Success | ||
Himawari 5 | ||||||||
F4 | August 17, 1996 01:53 |
H-II | LA-Y1, Tanegashima | ADEOS (Advanced Earth Observing Satellite) / Fuji OSCAR 29, JAS-2 | LEO | Success | ||
Midori, Fuji 3 | ||||||||
F6 | November 27, 1997 21:27 |
H-II | LA-Y1, Tanegashima | TRMM (Tropical Rainfall Measuring Mission) / ETS-VII (Engineering Test Satellite-VII) | LEO | Success | ||
Kiku 7 (Orihime & Hikoboshi) | ||||||||
F5 | February 21, 1998 07:55 |
H-II | LA-Y1, Tanegashima | COMETS (Communications and Broadcasting Engineering Test Satellites) | GEO | Partial failure | ||
Kakehashi, Faulty brazing in second-stage engine cooling system caused engine burn through and cable damage resulting in shutdown midway through the upper stage's second burn, leaving spacecraft in elliptical LEO instead of GTO. Spacecraft thrusters raised orbit enough to complete some communications experiments. | ||||||||
F8 | November 15, 1999 07:29 |
H-II | LA-Y1, Tanegashima | MTSAT (Multi-functional Transport Satellite) | GEO | Failure | ||
Cavitation in the first stage hydrogen turbopump impeller caused an impeller blade to fracture, resulting in loss of fuel and rapid shutdown of the engine at T+239 s. The vehicle impacted the ocean 380 km NW of Chichi-jima. | ||||||||
2001 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
TF1 | August 29, 2001 07:00:00 |
H-IIA 202 | LA-Y1, Tanegashima | VEP 2 / LRE | Success | |||
2002 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
TF2 | February 4, 2002 02:45:00 |
H-IIA 2024 | LA-Y1, Tanegashima | VEP 3 / MDS-1 (Tsubasa) / DASH | Success | |||
F3 | September 10, 2002 08:20:00 |
H-IIA 2024 | LA-Y1, Tanegashima | USERS / DRTS (Kodama) | Success | |||
F4 | December 14, 2002 01:31:00 |
H-IIA 202 | LA-Y1, Tanegashima | ADEOS 2 (Midori 2) / WEOS (Kanta-kun) / FedSat 1 / Micro LabSat 1 | Success | |||
2003 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F5 | March 28, 2003 01:27:00 |
H-IIA 2024 | LA-Y1, Tanegashima | IGS-Optical 1 / IGS-Radar 1 | Success | |||
F6 | November 29, 2003 04:33:00 |
H-IIA 2024 | LA-Y1, Tanegashima | IGS-Optical (2) / IGS-Radar (2) | Failure | |||
A hot gas leak from one SRB-A motor destroyed its separation system. The strap-on did not separate as planned, and the weight of the spent motor prevented the vehicle from achieving its planned height.[1] | ||||||||
2005 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F7 | February 26, 2005 09:25:00 |
H-IIA 2022 | LA-Y1, Tanegashima | MTSAT-1R (Himawari 6) | Success | |||
2006 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F8 | January 24, 2006 01:33:00 |
H-IIA 2022 | LA-Y1, Tanegashima | ALOS (Daichi) | Success | |||
F9 | February 18, 2006 06:27:00 |
H-IIA 2024 | LA-Y1, Tanegashima | MTSAT-2 (Himawari 7) | Success | |||
F10 | September 11, 2006 04:35:00 |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Optical 2 | Success | |||
F11 | December 18, 2006 06:32:00 |
H-IIA 204 | LA-Y1, Tanegashima | ETS-VIII (Kiku 8)[2] | GTO | Success | ||
2007 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F12 | February 24, 2007 04:41:00 |
H-IIA 2024 | LA-Y1, Tanegashima | IGS-Radar 2 / IGS-Optical 3V | Success | |||
F13 | September 14, 2007 01:31:01 |
H-IIA 2022 | LA-Y1, Tanegashima | SELENE (Kaguya) | Success | |||
2008 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F14 | February 23, 2008 08:55:00 |
H-IIA 2024 | LA-Y1, Tanegashima | WINDS (Kizuna) | Success | |||
2009 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F15 | January 23, 2009 03:54:00 |
H-IIA 202 | LA-Y1, Tanegashima | GOSAT (Ibuki) / SDS-1 / STARS (Kūkai) / KKS-1 (Kiseki) / PRISM (Hitomi) / Sohla-1 (Maido 1) / SORUNSAT-1 (Kagayaki) / SPRITE-SAT (Raijin) | Success[3] | |||
TF1 | 10 September 2009 17:01:46 |
H-IIB | LA-Y2, Tanegashima | HTV-1 | Success | |||
First flight of H-IIB | ||||||||
F16 | November 28, 2009 01:21:00 [4] |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Optical 3 | Success | |||
2010 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F17 | May 20, 2010 21:58:22[5][6][7] |
H-IIA 202[8] | LA-Y1, Tanegashima | PLANET-C (Akatsuki) / IKAROS / UNITEC-1 (Shin'en) / Waseda-SAT2 / K-Sat (Hayato) / Negai☆″ | Success | |||
F18 | September 11, 2010 11:17:00[9] |
H-IIA 202 | LA-Y1, Tanegashima | QZS-1 (Michibiki) | Success | |||
2011 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F2 | 22 January 2011 05:37:57 |
H-IIB | LA-Y2, Tanegashima | HTV-2 (Kounotori 2) | Success | |||
F19 | September 23, 2011 04:36:50[10] |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Optical 4 | Success | |||
F20 | December 12, 2011 01:21:00[11] |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Radar 3 | Success | |||
2012 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F21 | May 17, 2012 16:39:00 |
H-IIA 202[12] | LA-Y1, Tanegashima | GCOM-W1 (Shizuku) / KOMPSAT-3 (Arirang 3) / SDS-4 / HORYU-2 | Success | |||
F3 | 21 July 2012 02:06:18 |
H-IIB | LA-Y2, Tanegashima | HTV-3 (Kounotori 3) / Raiko / We Wish / Niwaka / TechEdSat / F-1 | Success | |||
CubeSats carried aboard HTV, on 4 October 2012 deployed from the ISS | ||||||||
2013 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F22 | January 27, 2013 04:40:00 |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Radar 4 / IGS-Optical 5V | Success | |||
F4 | 3 August 2013 19:48:46 |
H-IIB | LA-Y2, Tanegashima | HTV-4 (Kounotori 4) / Pico Dragon / ArduSat-1 / ArduSat-X / TechEdSat-3 | Success | |||
CubeSats carried aboard HTV for deployment from the ISS | ||||||||
2014 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F23 | February 27, 2014 18:37:00 |
H-IIA 202 | LA-Y1, Tanegashima | GPM-Core / SindaiSat (Ginrei) / STARS-II (Gennai) / TeikyoSat-3 / ITF-1 (Yui) / OPUSAT (CosMoz) / INVADER / KSAT2 | Success | |||
F24 | May 24, 2014 03:05:14 |
H-IIA 202 | LA-Y1, Tanegashima | ALOS-2 (Daichi 2) / RISING-2 / UNIFORM-1 / SOCRATES / SPROUT | Success | |||
F25 | October 7, 2014 05:16:00 |
H-IIA 202 | LA-Y1, Tanegashima | Himawari 8 | Success | |||
F26 | December 3, 2014 04:22:04 |
H-IIA 202 | LA-Y1, Tanegashima | Hayabusa 2 / Shin'en 2 / ARTSAT2-DESPATCH / PROCYON | Success | |||
2015 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F27 | February 1, 2015 01:21:00 |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Radar Spare | Success | |||
F28 | March 26, 2015 01:21:00 |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Optical 5 | Success | |||
F5 | 19 August 2015 11:50:49 |
H-IIB | LA-Y2, Tanegashima | HTV-5 (Kounotori 5) / SERPENS / S-CUBE / Flock-2b x 14 / GOMX-3 / AAUSAT5 | Success | |||
CubeSats carried aboard HTV for deployment from the ISS | ||||||||
F29 | November 24, 2015 06:50:00 |
H-IIA 204 | LA-Y1, Tanegashima | Telstar 12 Vantage[2] | GTO | Success | ||
2016 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F30 | February 17, 2016 08:45:00 |
H-IIA 202 | LA-Y1, Tanegashima | ASTRO-H (Hitomi) / ChubuSat-2 (Kinshachi 2) / ChubuSat-3 (Kinshachi 3) / Horyu-4 | Success | |||
The Hitomi telescope broke apart 37 days after launch.[13] | ||||||||
F31 | November 2, 2016 06:20:00 |
H-IIA 202 | LA-Y1, Tanegashima | Himawari 9 | Success | |||
F6 | 9 December 2016 13:26:47 |
H-IIB | LA-Y2, Tanegashima | HTV-6 (Kounotori 6) / AOBA-Velox III / TuPOD / EGG / ITF-2 / STARS-C / FREEDOM / WASEDA-SAT3 | Success | |||
CubeSats carried aboard HTV for deployment from the ISS | ||||||||
2017 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F32 | January 24, 2017 07:44:00 |
H-IIA 204 | LA-Y1, Tanegashima | DSN-2 (Kirameki 2)[2] | GTO | Success | ||
F33 | March 17, 2017 01:20:00 |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Radar 5 | Success | |||
F34 | June 1, 2017 00:17:46 |
H-IIA 202 | LA-Y1, Tanegashima | QZS-2 (Michibiki 2) | Success | |||
F35 | August 19, 2017 05:29:00 |
H-IIA 204 | LA-Y1, Tanegashima | QZS-3 (Michibiki 3) [2] | GTO | Success | ||
F36 | October 9, 2017 22:01:37 |
H-IIA 202 | LA-Y1, Tanegashima | QZS-4 (Michibiki 4) | Success | |||
F37 | December 23, 2017 01:26:22 |
H-IIA 202 | LA-Y1, Tanegashima | GCOM-C (Shikisai) / SLATS (Tsubame) | Success | |||
2018 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F38 | February 27, 2018 04:34:00 |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Optical 6 | Success | |||
F39 | June 12, 2018 04:20:00 |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Radar 6 | Success | |||
F7 | September 22, 2018 17:52:27 |
H-IIB | LA-Y2, Tanegashima | HTV-7 (Kounotori 7) / SPATIUM-I /RSP-00/ STARS-Me | Success | |||
CubeSats carried aboard HTV for deployment from the ISS | ||||||||
F40 | October 29, 2018 04:08:00 |
H-IIA 202 | LA-Y1, Tanegashima | GOSAT-2 (Ibuki-2) / KhalifaSat / Ten-Koh / Diwata-2B / Stars-AO (Aoi) / AUTcube2 (GamaCube) | Success | |||
2019 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F8 | September 24, 2019 16:05:05 |
H-IIB | LA-Y2, Tanegashima | HTV 8 (Kounotori 8) / NARSSCube-1 / AQT-D / RWASAT-1 | Success | |||
CubeSats carried aboard HTV for deployment from the ISS | ||||||||
2020 | ||||||||
Flight № | Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Payload mass | Orbit | Users | Launch outcome |
F41 | February 9, 2020 01:34:00 |
H-IIA 202 | LA-Y1, Tanegashima | IGS-Optical 7 | Success | |||
F9 | 20 May 2020 17:31:00 |
H-IIB | LA-Y2, Tanegashima | HTV-9 | Success | |||
Kounotori 9 HTV launch to the ISS. The last launch of both the carrier rocket and vehicle, awaiting new fleet of HTV-X and H3. | ||||||||
Planned launches
Date / time (UTC) | Rocket, Configuration |
Launch site | Payload | Orbit | Customer |
---|---|---|---|---|---|
July 14, 2020 20:51:27[14] | H-IIA 202 | Yoshinobu Launch Complex | Mars Hope | ||
2020 | H-IIA 202 | Yoshinobu Launch Complex | JDRS | ||
2020 | H-IIA 202 | Yoshinobu Launch Complex | IGS-Data Relay 1 | ||
2020 | H-IIA 202 | Yoshinobu Launch Complex | ALOS-3 | ||
2020 | H-IIA 202 | Yoshinobu Launch Complex | QZS-1R | ||
2020 | H-IIA 204 | Yoshinobu Launch Complex | Inmarsat-6 F1 | ||
2021 | H-IIA 202 | Yoshinobu Launch Complex | XRISM / SLIM | ||
2022 | H-IIA 202 | Yoshinobu Launch Complex | IGS-Radar 7 | ||
2023 | H-IIA 202 | Yoshinobu Launch Complex | IGS-Optical 8 | ||
2023 | H-IIA 202 | Yoshinobu Launch Complex | IGS-Radar 8 | ||
Final flight of H2A, and H2 family as a whole | |||||
Sources: Gunter's Space Page[15] and Japanese Cabinet[16]
References
- "Launch Result of IGS #2/H-IIA F6". JAXA. November 29, 2003. Retrieved June 19, 2013.
- Space Launch Report: H-IIA/B Data Sheet. Retrieved 20 Feb. 2019.
- "Launch Result of the IBUKI (GOSAT) by H-IIA Launch Vehicle No. 15". MHI and JAXA. January 23, 2009.
- "H-IIA F16". Sorae. Archived from the original on 2012-01-21.
- "Launch Day of the H-IIA Launch Vehicle No. 17". JAXA. March 3, 2010.
- "Overview of Secondary Payloads". JAXA.
- Tariq Malik (18 May 2010). "New Venus Probe to Launch Thursday From Japan After". space.com. Retrieved 20 May 2010.
- Chris Bergin (17 May 2010). "JAXA launch H-IIA carrying AKATSUKI and IKAROS scrubbed". NASASpacflight.com. Retrieved 17 May 2010.
- "New Launch Day of the First Quasi-Zenith Satellite 'MICHIBIKI' by H-IIA Launch Vehicle No. 18". JAXA.
- Chris Bergin (23 September 2011). "Japanese H-2A launches with new IGS military satellite". NASASpaceflight.com.
- Chris Bergin (11 December 2011). "Japanese H-2A lofts IGS (Radar-3) satellite into orbit". NASASpaceflight.com.
- "Launch Overview – H-IIA Launch Services Flight No.21". Mitsubishi Heavy Industries. Retrieved April 15, 2012.
- Clark, Stephen (18 April 2016). "Attitude control failures led to break-up of Japanese astronomy satellite". Spaceflight Now. Retrieved 21 April 2016.
- "SpaceFlight Now Launch Schedule". Retrieved 19 May 2020.
- Krebs, Gunter. "H-2A". Gunter's Space Page. Retrieved 19 August 2017.
- "宇宙基本計画工程表 (平成29年度改訂)" (PDF) (in Japanese). Cabinet Office. 12 December 2017. Retrieved 2017-12-29.
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