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Mu-3H

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M-3H

Mu-3H
1:110 Scale
H:21.6 cmD:1.3 cm
~23 bricks tall~2 studs wide
Maiden Launch1977-02-19
Family: Mu
Designer: ISAS·Manufacturer: MHI·Operator: JAXA·Commissioner: ISAS
3–4 Stages
Height / Length
23.8 m
Diameter
1.4 m
Launch Mass
48,700 kg
Takeoff Thrust
1,060 kN
LEO Capacity
300 kg

Mission Profile

Mu-3H (M-3H) is a three- to four-stage solid-propellant Japanese launch vehicle developed by the Institute of Space and Astronautical Science. First flying on 19 February 1977, it stood 23.8 meters tall with a 300 kg LEO capacity and was used to launch scientific and solar observation satellites. The Mu rocket family made Japan a pioneer in solid-propellant orbital launch capability.

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