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H3·Mitsubishi Heavy Industries

H3

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Specifications

Status
active
Height
63 m
Diameter
5.27 m
Mass
574,000 kg
Stages
2
Thrust
2,942 kN
Payload to GTO
6,500 kg
First flight
2028-03-31
Total launches
0
Success / Fail
0 / 0

The H3 Launch Vehicle is an expendable launch system in development in Japan. H3 rockets are liquid-propellant rockets with strap-on solid rocket boosters and are planned to be launched from the Tanegashima Space Center in Japan. Mitsubishi and the JAXA have been responsible for the design, manufacture, and operation of the H3.

Propulsion

First stage

2×LE-91,471 kN
LH2 / LOX · expander-bleed
Mitsubishi / IHIIsp 425s (vac)since 20242 or 3

Second stage

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