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Space · launch vehicle

H-IIA 202

MHI RETIRED
At a glance
Launches
35
Success rate
100%
35 ok · 0 failed
Payload to LEO
10,000 kg
Payload to GTO
4,100 kg
Status
Retired
First flight
29 Aug 2001
Reusable
No
Height
53 m
Diameter
4 m
Launch mass
285 t
Liftoff thrust
2,260 kN
Stages
2
Launch cost
$90,000,000
Booster landings
—
About

H-IIA (H2A) is an active 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.