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H-II · Mitsubishi Heavy Industries

H-IIA 204

retired
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Specifications

Status
retired
Height
53 m
Diameter
4 m
Mass
445,000 kg
Stages
2
Payload to GTO
6,000 kg
First flight
2006-12-18
Total launches
5
Success / Fail
5 / 0

H-IIA (H2A) was an expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The liquid-fueled H-IIA rockets have been used to launch satellites into geostationary orbit, to launch a lunar orbiting spacecraft, and to launch Akatsuki, which studied the planet Venus. Launches occur at the Tanegashima Space Center.

Propulsion

First stage

LE-7A870 kN
LH2 / LOX · staged-combustion
Mitsubishi / IHIIsp 440s (vac)since 2001

Second stage

LE-5B137 kN
LH2 / LOX · expander-bleed
MitsubishiIsp 447s (vac)since 2001

Payloads it launched · 5

INMARSAT 6-F1
GEO
QZS-3 (MICHIBIKI-3)
GEO
DSN-2
Payload
TELSTAR 12V
GEO
KIKU-8 (ETS-VIII)
GEO