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H-II · Mitsubishi Heavy Industries

H-IIA 2024

retired
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Specifications

Status
retired
Height
53 m
Diameter
4 m
Mass
347,000 kg
Stages
2
Payload to GTO
5,000 kg
First flight
2002-02-04
Total launches
7
Success / Fail
6 / 1

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.

Payloads it launched · 11

KIZUNA (WINDS)
GEO
IGS 4B
LEO
IGS 4A
LEO
HIMAWARI-7 (MTSAT-2)
GEO
IGS 1A
Payload
IGS 1B
LEO
USERS REM
LEO
USERS SEM
LEO
KODAMA (DRTS)
GEO
DASH & VEP 3
HEO
TSUBASA (MDS-1)
MEO