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Space · launch vehicle

H-IIA 2022

MHI RETIRED
At a glance
Launches
3
Success rate
100%
3 ok · 0 failed
Payload to LEO
—
Payload to GTO
4,500 kg
Status
Retired
First flight
26 Feb 2005
Reusable
No
Height
53 m
Diameter
4 m
Launch mass
316 t
Liftoff thrust
—
Stages
2
Launch cost
—
Booster landings
—
About

The H-IIA rocket family is an expendable launch system operated by Mitsubishi Heavy Industries for the Japan Aerospace Exploration Agency. The liquid fuelled rocket has been used to launch satellites, lunar spacecraft and planetary science craft.