H-IIA: Difference between revisions

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Launch history: Launch delayed
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| H2A 204||445||6||4 SRB-A (SRB)
| H2A 204||445||6||4 SRB-A (SRB)
|-style="background: #e0e0e0
|-style="background: #e0e0e0
| H2A 212 ||403||7.5||2 SRB-A (SRB) + 1 LRB <ref name="SpaceDaily">{{cite web|url=https://www.spacedaily.com/reports/Japan_Reenters_Rocket_Race_With_New_Improved_H2A.html|title=Japan Reenters Rocket Race With New Improved H2A|publisher=Space Daily|date=20 August 2001}}</ref><ref>{{Cite web|url=https://space.skyrocket.de/doc_lau/h-2a.htm|title = H-2A}}</ref>
| H2A 212 ||403||7.5||2 SRB-A (SRB) + 1 LRB<ref name="SpaceDaily">{{cite web|url=https://www.spacedaily.com/reports/Japan_Reenters_Rocket_Race_With_New_Improved_H2A.html|title=Japan Reenters Rocket Race With New Improved H2A|publisher=Space Daily|date=20 August 2001}}</ref><ref>{{Cite web|url=https://space.skyrocket.de/doc_lau/h-2a.htm|title = H-2A}}</ref>
|-style="background: #e0e0e0
|-style="background: #e0e0e0
| H2A 222 ||520||9.5||2 SRB-A (SRB) + 2 LRBs <ref name="SpaceDaily"/>
| H2A 222 ||520||9.5||2 SRB-A (SRB) + 2 LRBs<ref name="SpaceDaily"/>
|}
|}


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|-
|-
| F15
| F15
| 23 January 2009<br/>03:54:00 || H2A 202 || [[GOSAT]] (Ibuki)<br/>[[SDS-1]]<br/>STARS (Kūkai)<br/>KKS-1 (Kiseki)<br/>PRISM (Hitomi)<br/>[[Sohla]]-1 (Maido 1)<br/>SORUNSAT-1 (Kagayaki)<br/>SPRITE-SAT (Raijin) || {{Success}} <ref>{{cite web|url=http://www.jaxa.jp/press/2009/01/20090123_h2a-f15_e.html|title=Launch Result of the IBUKI (GOSAT) by H-IIA Launch Vehicle No. 15|date=January 23, 2009|publisher=MHI and JAXA|access-date=24 January 2009|archive-date=21 June 2013|archive-url=https://web.archive.org/web/20130621105225/http://www.jaxa.jp/press/2009/01/20090123_h2a-f15_e.html|url-status=dead}}</ref>
| 23 January 2009<br/>03:54:00 || H2A 202 || [[GOSAT]] (Ibuki)<br/>[[SDS-1]]<br/>STARS (Kūkai)<br/>KKS-1 (Kiseki)<br/>PRISM (Hitomi)<br/>[[Sohla]]-1 (Maido 1)<br/>SORUNSAT-1 (Kagayaki)<br/>SPRITE-SAT (Raijin) || {{Success}}<ref>{{cite web|url=http://www.jaxa.jp/press/2009/01/20090123_h2a-f15_e.html|title=Launch Result of the IBUKI (GOSAT) by H-IIA Launch Vehicle No. 15|date=January 23, 2009|publisher=MHI and JAXA|access-date=24 January 2009|archive-date=21 June 2013|archive-url=https://web.archive.org/web/20130621105225/http://www.jaxa.jp/press/2009/01/20090123_h2a-f15_e.html|url-status=dead}}</ref>


|-
|-
| F16
| F16
| 28 November 2009<br/>01:21:00 <ref>{{cite web|url=http://www.sorae.jp/030801/3328.html|title=H-IIA F16|publisher=Sorae|url-status=dead |archive-url=https://web.archive.org/web/20120218012627/http://www.sorae.jp/030801/3328.html|archive-date=2012-02-18}}</ref>|| H2A 202|| [[Information Gathering Satellite|IGS-Optical 3]] || {{Success}}
| 28 November 2009<br/>01:21:00<ref>{{cite web|url=http://www.sorae.jp/030801/3328.html|title=H-IIA F16|publisher=Sorae|url-status=dead |archive-url=https://web.archive.org/web/20120218012627/http://www.sorae.jp/030801/3328.html|archive-date=2012-02-18}}</ref>|| H2A 202|| [[Information Gathering Satellite|IGS-Optical 3]] || {{Success}}


|-
|-
| F17
| F17
| 20 May 2010<br/>21:58:22 <ref>{{cite web|url=http://www.jaxa.jp/press/2010/03/20100303_h2af17_e.html|title=Launch Day of the H-IIA Launch Vehicle No. 17|date=March 3, 2010|publisher=JAXA|access-date=8 March 2010|archive-date=3 June 2013|archive-url=https://web.archive.org/web/20130603022829/http://www.jaxa.jp/press/2010/03/20100303_h2af17_e.html|url-status=dead}}</ref><ref>{{cite web|url=http://www.jaxa.jp/countdown/f17/overview/sub_payload_e.html|title=Overview of Secondary Payloads|publisher=JAXA}}</ref><ref>{{cite web|url=http://www.space.com/missionlaunches/japan-venus-probe-launch-thursday-100518.html|title=New Venus Probe to Launch Thursday From Japan After|website=space.com|author=Tariq Malik|date=18 May 2010|access-date=20 May 2010}}</ref>|| H2A 202 <ref name="nasa_f17">{{cite web |url=http://www.nasaspaceflight.com/2010/05/axa-launch-h-iia-carrying-akatsuki-ikaros/|title=JAXA launch H-IIA carrying AKATSUKI and IKAROS scrubbed|author=Chris Bergin|date=17 May 2010|access-date=17 May 2010 |publisher=NASASpaceflight}}</ref> || [[PLANET-C]] (Akatsuki)<br/>[[IKAROS]]<br/>[[UNITEC-1]] (Shin'en)<br/>[[Waseda-SAT2]]<br/>[[K-Sat]] (Hayato)<br/>[[Negai (satellite)|Negai☆″]]|| {{Success}}
| 20 May 2010<br/>21:58:22<ref>{{cite web|url=http://www.jaxa.jp/press/2010/03/20100303_h2af17_e.html|title=Launch Day of the H-IIA Launch Vehicle No. 17|date=March 3, 2010|publisher=JAXA|access-date=8 March 2010|archive-date=3 June 2013|archive-url=https://web.archive.org/web/20130603022829/http://www.jaxa.jp/press/2010/03/20100303_h2af17_e.html|url-status=dead}}</ref><ref>{{cite web|url=http://www.jaxa.jp/countdown/f17/overview/sub_payload_e.html|title=Overview of Secondary Payloads|publisher=JAXA}}</ref><ref>{{cite web|url=http://www.space.com/missionlaunches/japan-venus-probe-launch-thursday-100518.html|title=New Venus Probe to Launch Thursday From Japan After|website=space.com|author=Tariq Malik|date=18 May 2010|access-date=20 May 2010}}</ref>|| H2A 202<ref name="nasa_f17">{{cite web |url=http://www.nasaspaceflight.com/2010/05/axa-launch-h-iia-carrying-akatsuki-ikaros/|title=JAXA launch H-IIA carrying AKATSUKI and IKAROS scrubbed|author=Chris Bergin|date=17 May 2010|access-date=17 May 2010 |publisher=NASASpaceflight}}</ref> || [[PLANET-C]] (Akatsuki)<br/>[[IKAROS]]<br/>[[UNITEC-1]] (Shin'en)<br/>[[Waseda-SAT2]]<br/>[[K-Sat]] (Hayato)<br/>[[Negai (satellite)|Negai☆″]]|| {{Success}}


|-
|-
| F18
| F18
| 11 September 2010<br/>11:17:00 <ref>{{cite web|url=http://www.jaxa.jp/press/2010/08/20100804_michibiki_e.html|title=New Launch Day of the First Quasi-Zenith Satellite 'MICHIBIKI' by H-IIA Launch Vehicle No. 18|publisher=JAXA}}</ref>|| H2A 202 || [[Quasi-Zenith Satellite System|QZS-1]] (Michibiki) || {{Success}}
| 11 September 2010<br/>11:17:00<ref>{{cite web|url=http://www.jaxa.jp/press/2010/08/20100804_michibiki_e.html|title=New Launch Day of the First Quasi-Zenith Satellite 'MICHIBIKI' by H-IIA Launch Vehicle No. 18|publisher=JAXA}}</ref>|| H2A 202 || [[Quasi-Zenith Satellite System|QZS-1]] (Michibiki) || {{Success}}


|-
|-
| F19
| F19
| 23 September 2011<br/>04:36:50 <ref>{{cite web|url=http://www.nasaspaceflight.com/2011/09/japanese-h-2a-launches-new-igs-military-satellite/|title=Japanese H-2A launches with new IGS military satellite |author=Chris Bergin|date=23 September 2011|publisher=NASASpaceflight}}</ref>|| H2A 202 || [[Information Gathering Satellite|IGS-Optical 4]] || {{Success}}
| 23 September 2011<br/>04:36:50<ref>{{cite web|url=http://www.nasaspaceflight.com/2011/09/japanese-h-2a-launches-new-igs-military-satellite/|title=Japanese H-2A launches with new IGS military satellite |author=Chris Bergin|date=23 September 2011|publisher=NASASpaceflight}}</ref>|| H2A 202 || [[Information Gathering Satellite|IGS-Optical 4]] || {{Success}}


|-
|-
| F20
| F20
| 12 December 2011<br/>01:21:00 <ref>{{cite web|url=http://www.nasaspaceflight.com/2011/12/japanese-h-2a-lofts-igs-radar-3-satellite-into-orbit/|author=Chris Bergin|date=11 December 2011
| 12 December 2011<br/>01:21:00<ref>{{cite web|url=http://www.nasaspaceflight.com/2011/12/japanese-h-2a-lofts-igs-radar-3-satellite-into-orbit/|author=Chris Bergin|date=11 December 2011
|publisher=NASASpaceflight|title=Japanese H-2A lofts IGS (Radar-3) satellite into orbit}}</ref>|| H2A 202 || [[Information Gathering Satellite|IGS-Radar 3]] || {{Success}}
|publisher=NASASpaceflight|title=Japanese H-2A lofts IGS (Radar-3) satellite into orbit}}</ref>|| H2A 202 || [[Information Gathering Satellite|IGS-Radar 3]] || {{Success}}


|-
|-
| F21
| F21
| 17 May 2012<br/>16:39:00 || H2A 202 <ref>{{cite web|url=http://h2a.mhi.co.jp/en/f21/overview/index.html|title=Launch Overview – H-IIA Launch Services Flight No.21|access-date=April 15, 2012|publisher=Mitsubishi Heavy Industries|archive-date=15 October 2017|archive-url=https://web.archive.org/web/20171015164805/http://h2a.mhi.co.jp/en/f21/overview/index.html|url-status=dead}}</ref> || [[Global Change Observation Mission|GCOM-W1]] (Shizuku)<br/>[[KOMPSAT-3]] (Arirang 3)<br/>[[SDS-4]] <br/>[[HORYU-2]]|| {{Success}}
| 17 May 2012<br/>16:39:00 || H2A 202<ref>{{cite web|url=http://h2a.mhi.co.jp/en/f21/overview/index.html|title=Launch Overview – H-IIA Launch Services Flight No.21|access-date=April 15, 2012|publisher=Mitsubishi Heavy Industries|archive-date=15 October 2017|archive-url=https://web.archive.org/web/20171015164805/http://h2a.mhi.co.jp/en/f21/overview/index.html|url-status=dead}}</ref> || [[Global Change Observation Mission|GCOM-W1]] (Shizuku)<br/>[[KOMPSAT-3]] (Arirang 3)<br/>[[SDS-4]] <br/>[[HORYU-2]]|| {{Success}}


|-
|-
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|-
|-
| rowspan=2|F50
| rowspan=2|F50
| 23 June 2025<br/>16:33 || H2A 202 || [[GOSAT-GW]]  || {{Planned}}
| June 2025<br/> || H2A 202 || [[GOSAT-GW]]  || {{Planned}}
|-
|-
| colspan=4 style="background:linen;" | Final flight of H-IIA, and H-II family as a whole.
| colspan=4 style="background:linen;" | Final flight of H-IIA, and H-II family as a whole.

Revision as of 13:55, 19 June 2025

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File:H-IIA F19 launching IGS-O4.jpg
The Liftoff of H-IIA Flight 19
File:H-IIA Family.png
The H-IIA rocket lineup
File:H-IIA-Launch-Vehicle.png
The H-IIA
File:At Tokyo 2024 379.jpg
Engine at Miraikan

H-IIA (H-2A) is an active expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. These liquid fuel rockets have been used to launch satellites into geostationary orbit; lunar orbiting spacecraft; Akatsuki, which studied the planet Venus; and the Emirates Mars Mission, which was launched to Mars in July 2020. Launches occur at the Tanegashima Space Center. The H-IIA first flew in 2001. Template:As of, H-IIA rockets were launched 49 times, including 43 consecutive missions without a failure, dating back to 29 November 2003.

Production and management of the H-IIA shifted from JAXA to MHI on 1 April 2007. Flight 13, which launched the lunar orbiter SELENE, was the first H-IIA launched after this privatization.[1]

The H-IIA is a derivative of the earlier H-II rocket, substantially redesigned to improve reliability and minimize costs. There have been four variants, with two in active service (as of 2020) for various purposes. A derivative design, the H-IIB, was developed in the 2000s and made its maiden flight in 2009 before finally retired on its final launch in 2020.

Vehicle description

The base configuration, and the only remaining active configuration of an H-IIA launch vehicle, uses two SRB-A type solid rocket boosters (SRBs). The launch capability of the H-IIA launch vehicle could be enhanced by adding an additional two SRB-A boosters or up to four Castor 4AXL solid strap-on boosters (SSBs).

The models are indicated by three or four numbers following the prefix "H2A":[2]

  • The first number in the sequence indicates the number of stages (always 2)
  • The second number in the sequence indicates the number of liquid rocket boosters (a planned addition to the launch vehicle that was canceled, so always 0)
  • The third number in the sequence indicates the number of SRB-A type solid rocket boosters (2 or 4)
  • The fourth, optional, number in the sequence indicates the number of Castor 4AXL solid strap-on boosters (2 or 4)

Variants

Launch system status

<templatestyles src="Legend/styles.css" />

  Active

<templatestyles src="Legend/styles.css" />

  Discontinued

<templatestyles src="Legend/styles.css" />

  Cancelled
Designation Mass (tonnes) Payload to GTO (tonnes) Addon modules
H2A 202 285 4.1 2 SRB-A (SRB)
H2A 2022[3] 316 4.5 2 SRB-A (SRB) + 2 Castor 4AXL (SSB)
H2A 2024 347 5 2 SRB-A (SRB) + 4 Castor 4AXL (SSB)
H2A 204 445 6 4 SRB-A (SRB)
H2A 212 403 7.5 2 SRB-A (SRB) + 1 LRB[4][5]
H2A 222 520 9.5 2 SRB-A (SRB) + 2 LRBs[4]

Launch history

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The first H-IIA was successfully launched on 29 August 2001, followed by a string of successes.

The sixth launch on 29 November 2003, intended to launch two IGS reconnaissance satellites, failed. JAXA announced that launches would resume in 2005, and the first successful flight took place on 26 February 2005 with the launch of MTSAT-1R.

The first launch for a mission beyond Earth orbit was on 14 September 2007 for the SELENE Moon mission. The first foreign payload on the H-IIA was the Australian FedSat-1 in 2002. As of March 2015, 27 out of 28 launches were successful.

A rocket with increased launch capabilities, H-IIB, is a derivative of the H-IIA family. H-IIB uses two LE-7A engines in its first stage, as opposed to one in H-IIA. The first H-IIB was successfully launched on 10 September 2009.

For the 29th flight on 24 November 2015, an H-IIA with an upgraded second stage[6] launched the Telstar 12V satellite, the first commercial primary payload for a Japanese launch vehicle.[7]

Flight

No.

Date (UTC) Type Payload(s) Outcome
TF1 29 August 2001
07:00:00
H2A 202 VEP 2
LRE
Template:Success
TF2 4 February 2002
02:45:00
H2A 2024 VEP 3
MDS-1 (Tsubasa)
DASH
Template:Success
F3 10 September 2002
08:20:00
H2A 2024 USERS
DRTS (Kodama)
Template:Success
F4 14 December 2002
01:31:00
H2A 202 ADEOS 2 (Midori 2)
WEOS (Kanta-kun)
FedSat 1
Micro LabSat 1
Template:Success
F5 28 March 2003
01:27:00
H2A 2024 IGS-Optical 1
IGS-Radar 1
Template:Success
F6 29 November 2003
04:33:00
H2A 2024 IGS-Optical
IGS-Radar
Template:Failure
A hot gas leak from SRB-A motor destroyed its separation system and the booster did not separate as planned. The weight of the spent motor prevented the vehicle from achieving its planned speed and height and it was destroyed via a ground command about 10 minutes into the flight.[8]
F7 26 February 2005
09:25:00
H2A 2022 MTSAT-1R (Himawari 6) Template:Success
F8 24 January 2006
01:33:00
H2A 2022 ALOS (Daichi) Template:Success
F9 18 February 2006
06:27:00
H2A 2024 MTSAT-2 (Himawari 7) Template:Success
F10 11 September 2006
04:35:00
H2A 202 IGS-Optical 2 Template:Success
F11 18 December 2006
06:32:00
H2A 204 ETS-VIII (Kiku 8) Template:Success
F12 24 February 2007
04:41:00
H2A 2024 IGS-Radar 2
IGS-Optical 3V
Template:Success
F13 14 September 2007
01:31:01
H2A 2022 SELENE (Kaguya) Template:Success
F14 23 February 2008
08:55:00
H2A 2024 WINDS (Kizuna) Template:Success
F15 23 January 2009
03:54:00
H2A 202 GOSAT (Ibuki)
SDS-1
STARS (Kūkai)
KKS-1 (Kiseki)
PRISM (Hitomi)
Sohla-1 (Maido 1)
SORUNSAT-1 (Kagayaki)
SPRITE-SAT (Raijin)
Template:Success[9]
F16 28 November 2009
01:21:00[10]
H2A 202 IGS-Optical 3 Template:Success
F17 20 May 2010
21:58:22[11][12][13]
H2A 202[14] PLANET-C (Akatsuki)
IKAROS
UNITEC-1 (Shin'en)
Waseda-SAT2
K-Sat (Hayato)
Negai☆″
Template:Success
F18 11 September 2010
11:17:00[15]
H2A 202 QZS-1 (Michibiki) Template:Success
F19 23 September 2011
04:36:50[16]
H2A 202 IGS-Optical 4 Template:Success
F20 12 December 2011
01:21:00[17]
H2A 202 IGS-Radar 3 Template:Success
F21 17 May 2012
16:39:00
H2A 202[18] GCOM-W1 (Shizuku)
KOMPSAT-3 (Arirang 3)
SDS-4
HORYU-2
Template:Success
F22 27 January 2013
04:40:00
H2A 202 IGS-Radar 4
IGS-Optical 5V
Template:Success
F23 27 February 2014
18:37:00
H2A 202 GPM-Core
SindaiSat (Ginrei)
STARS-II (Gennai)
TeikyoSat-3
ITF-1 (Yui)
OPUSAT (CosMoz)
INVADER
KSAT2
Template:Success
F24 24 May 2014
03:05:14
H2A 202 ALOS-2 (Daichi 2)
RISING-2
UNIFORM-1
SOCRATES
SPROUT
Template:Success
F25 7 October 2014
05:16:00
H2A 202 Himawari 8 Template:Success
F26 3 December 2014
04:22:04
H2A 202 Hayabusa2
Shin'en 2
ARTSAT2-DESPATCH
PROCYON
Template:Success
F27 1 February 2015
01:21:00
H2A 202 IGS-Radar Spare Template:Success
F28 26 March 2015
01:21:00
H2A 202 IGS-Optical 5 Template:Success
F29 24 November 2015
06:50:00
H2A 204 Telstar 12 Vantage Template:Success
F30 17 February 2016
08:45:00
H2A 202 ASTRO-H (Hitomi)
ChubuSat-2 (Kinshachi 2)
ChubuSat-3 (Kinshachi 3)
Horyu-4
Template:Success
The Hitomi telescope broke apart 37 days after launch.[19]
F31 2 November 2016
06:20:00
H2A 202 Himawari 9 Template:Success
F32 24 January 2017
07:44:00
H2A 204 DSN-2 (Kirameki 2) Template:Success
F33 17 March 2017
01:20:00
H2A 202 IGS-Radar 5 Template:Success
F34 1 June 2017
00:17:46
H2A 202 QZS-2 (Michibiki 2) Template:Success
F35 19 August 2017
05:29:00
H2A 204 QZS-3 (Michibiki 3) Template:Success
F36 9 October 2017
22:01:37
H2A 202 QZS-4 (Michibiki 4) Template:Success
F37 23 December 2017
01:26:22
H2A 202 GCOM-C (Shikisai)
SLATS (Tsubame)
Template:Success
F38 27 February 2018
04:34:00
H2A 202 IGS-Optical 6 Template:Success
F39 12 June 2018
04:20:00
H2A 202 IGS-Radar 6 Template:Success
F40 29 October 2018
04:08:00
H2A 202 GOSAT-2 (Ibuki-2)
KhalifaSat
Diwata-2B
Tenkōh
Stars-AO (Aoi)
AUTcube2 (Gamacube)
Template:Success
F41 9 February 2020
01:34:00
H2A 202 IGS-Optical 7 Template:Success
F42 19 July 2020
21:58:14
H2A 202 Emirates Mars Mission (Hope) Template:Success
F43 29 November 2020
07:25:00
H2A 202 JDRS/LUCAS Template:Success
F44 26 October 2021
02:19:37
H2A 202 QZS-1R Template:Success
F45 22 December 2021
15:32:00
H2A 204 Inmarsat-6 F1 Template:Success
F46 26 January 2023
01:50:21
H2A 202 IGS-Radar 7 Template:Success
F47 6 September 2023
23:42:11
H2A 202 XRISM
SLIM
Template:Success
F48 12 January 2024
04:44:26
H2A 202 IGS-Optical 8 Template:Success
F49 26 September 2024
05:24:20
H2A 202 IGS-Radar 8 Template:Success
F50 June 2025
H2A 202 GOSAT-GW Template:Planned
Final flight of H-IIA, and H-II family as a whole.

See also

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References

Notes Template:Reflist

Sources Template:Refbegin

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Template:Refend

External links

Template:Sister project

Template:Mitsubishi Heavy Industries Template:Expendable launch systems Template:Japanese launch systems

de:H-II#H-IIA

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