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H-IIA

From Wikipedia, the free encyclopedia

H-IIA
H-IIA rocket
H-IIA rocket
Fact sheet
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)
Payload to
GTO
202: 4,100 kg
2024: 5000 kg
(202: 9,000 lb
2024: 11,000 lb)
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
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
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
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

[edit] External links

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