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M-23-Mu

Engine · Japan

Original archive entry. The text, images and links below are kept as they were written.

Nissan solid rocket engine. Used on Mu-3S launch vehicle. First flight 1969. Mu-3S second stage.

Thrust (sl): 404.500 kN (90,935 lbf). Thrust (sl): 41,247 kgf.

Country
Japan
Launch Vehicles
Mu-3S, Mu-3S-II
Propellants
Solid
Stages
M-23-Mu
Agency
Nissan