H-IIA
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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.
Contents |
Basic specs
- Length: 53 m
- Stages: 2
Variants
Date (UTC) | Flight | Model | Payload | Result |
---|---|---|---|---|
29.08.2001 07:00:00 | TF1 | H2a202 | VEP 2 | Success |
LRE | ||||
04.02.2002 02:45:00 | TF2 | H2a2024 | VEP 3 | Success |
MDS 1 (Tsubasa) | ||||
DASH | ||||
10.09.2002 08:20:00 | 3F | H2a2024 | USERS | Success |
DRTS (Kodama) | ||||
14.12.2002 01:31:00 | 4F | H2a202 | ADEOS 2 | Success |
WEOS | ||||
FedSat 1 | ||||
Micro-Lab-Sat 1 | ||||
28.03.2003 01:27:00 | 5F | H2a2024 | IGS-Optical 1 | Success |
IGS-Radar 1 | ||||
29.11.2003 04:33:00 | 6F | H2a2024 | IGS-Optical 2 | Failure |
IGS-Radar 2 | ||||
26.02.2005 09:25:00 | 7F | H2a2022 | MTSat-1R | Success |
24.01.2006 01:33:00 | 8F | H2a2022 | ALOS | Success |
18.02.2006 06:27:00 | 9F | H2a2024 | MTSat-2 | Success |
Next flight, 10F is scheduled for no earlier than July 2006 with a pair of reconnaissance satellites. Maiden flight of the 204 version is around end of 2006 with the ETS-VIII.