H-IIA
From Wikipedia, the free encyclopedia
H-IIA rocket |
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Fact sheet | ||
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Function | Launch vehicle | |
Manufacturer | Mitsubishi Heavy Industries | |
Country of origin | Japan | |
Size | ||
Height | 53 m (173 ft) | |
Diameter | 4 m (13.1 ft) | |
Mass | 285,000 kg (628,000 lb) | |
Stages | 2 | |
Capacity | ||
Payload to LEO | 202: 10,000 kg 2024: 11,730 kg (202: 22,000 lb 2024: 25,860 lb) |
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Payload to GTO |
202: 4,100 kg 2024: 5000 kg (202: 9,000 lb 2024: 11,000 lb) |
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Launch History | ||
Status | Active | |
Launch Sites | LC-Y, Tanegashima | |
Total launches | 12 (202: 3, 204: 1, 2022: 2 , 2024: 6) | |
Successes | 11 (202: 3, 204: 1, 2022: 2 , 2024: 5) | |
Failures | 1 (2024) | |
Maiden flight | H-IIA 202: 29 August 2001 204: 18 December 2006 2022: 26 February 2005 2024: 4 February 2002 |
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Boosters (H-IIA 2022/2024) - Castor 4AXL | ||
No boosters | 2 - 4 | |
Engines | 1 Solid | |
Thrust | 745 kN | |
Specific Impulse | 283 sec | |
Burn time | 60 seconds | |
Fuel | Solid | |
Boosters (All Variants) - SRB-A | ||
No boosters | 2 - 4 | |
Engines | 1 Solid | |
Thrust | (2,250 kN) | |
Specific Impulse | 280 sec | |
Burn time | 120 seconds | |
Fuel | Solid | |
First Stage | ||
Engines | 1 LE-7A | |
Thrust | 1,098 kN (246,840 lbf) | |
Specific Impulse | 440 sec | |
Burn time | 390 seconds | |
Fuel | LOX/LH2 | |
Second Stage | ||
Engines | 1 LE-5B | |
Thrust | 137 kN (30,798 lbf) | |
Specific Impulse | 447 sec | |
Burn time | 534 seconds | |
Fuel | LOX/LH2 | |
The H-IIA is a family of liquid-fuelled rockets providing an expendable launch system for the purpose of launching satellites into geostationary orbit. It is manufactured by Mitsubishi and ATK Thiokol for the Japan Aerospace Exploration Agency, or JAXA. Launches occur at the Tanegashima Space Center.
The H-IIA is a derivative of the earlier H-II rocket, though has been substantially redesigned to improve reliability and minimize costs, after the H-II proved to be expensive and failure-prone. There are four different variants of the H-IIA for various purposes.
The H-IIA was first launched on August 29, 2001, and the sixth launch on November 29, 2003 failed. The rocket was intended to launch two reconnaissance satellites to observe North Korea. JAXA announced that launches would resume in 2005, and indeed the first successful flight took place on February 26 with the launch of MTSAT-1R.
Japan's eighth H-IIA launch was successful as well when the Advanced Land Observation Satellite (ALOS) was lofted into orbit to carry out a remote sensing mission in January 2006.
The first launch for a mission beyond Earth orbit will be in August 2007 for the SELENE moon mission.
As of February 2007, 11 attempts of 12 launches were successful.
JAXA now foresees increasing the diameter of the main cryogenic tank of the launcher in order to augment its performance. The resulting launcher, H-IIB, will fly in 2009.
Contents |
[edit] SPEC and Variants
Designation | Mass (tonnes) | Payload (tonnes to GTO) | Addon modules |
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H-IIA202 | 285 | 4 | 2 Solid rocket boosters (SRBs) |
H-IIA2022 | 316 | 4.5 | 2 SRBs + 2 Solid Strap-on Boosters (SSBs) |
H-IIA2024 | 347 | 5 | 2 SRBs + 4 SSBs |
H-IIA204 | 445 | 6 | 4 SRBs |
H-IIA212 (cancelled) | 403 | 7.5 | 2 SRBs + 1 Liquid Strap-On Booster (LRB) |
H-IIA222 (cancelled) | 520 | 9.5 | 2 SRBs + 2 LRBs |
[edit] H-IIA flights
Date (UTC) | Flight | Model | Payload | Result |
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August 29, 2001 07:00:00 | TF1 | HIIA202 | VEP 2 | Success |
LRE | ||||
February 4, 2002 02:45:00 | TF2 | HIIA2024 | VEP 3 | Success |
MDS1 (Tsubasa) | ||||
DASH | ||||
September 10, 2002 08:20:00 | F3 | HIIA2024 | USERS | Success |
DRTS (Kodama) | ||||
December 14, 2002 01:31:00 | F4 | HIIA202 | ADEOS 2 | Success |
WEOS | ||||
FedSat 1 | ||||
Micro-Lab-Sat 1 | ||||
March 28, 2003 01:27:00 | F5 | HIIA2024 | IGS-Optical 1 | Success |
IGS-Radar 1 | ||||
November 29, 2003 04:33:00 | F6 | HIIA2024 | IGS-Optical 2 | Failure |
IGS-Radar 2 | ||||
February 26, 2005 09:25:00 | F7 | HIIA2022 | MTSat-1R | Success |
January 24, 2006 01:33:00 | F8 | HIIA2022 | ALOS | Success |
February 18, 2006 06:27:00 | F9 | HIIA2024 | MTSat-2 | Success |
September 11, 2006 04:35:00 | F10 | HIIA202 | IGS-Optical 3 | Success |
December 18, 2006 06:32:00 | F11 | HIIA204 | ETS-VIII | Success |
February 24, 2007 04:41:00 | F12 | HIIA2024 | IGS-Radar 3 | Success |
IGS-Optical 4 |
[edit] References
- Japan Prepares for Crucial Rocket Launch. SPACE.com. Retrieved on 16 February 2005.
- H-IIA Expendable Launch Vehicle. SPACEandTECH. Retrieved on February 16, 2005.
[edit] External links
- Encyclopedia Astronautica page
- H-IIA English page
- JAXA English page
- H-llA LAUNCH SERVICES
- JAXA Launch Schedule
- Tanegashima Space Center
- "Tanegashima Space Center" -- VISIT JAXA --
- Failed Launch, 11-29-2003
- Image
- Launch 2 Image
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