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M-23-Mu
Part of M-10 Family
Nissan solid rocket engine. Used on Mu-3S launch vehicle. First flight 1969. Mu-3S second stage.

AKA: M-23;Mu-3S-2. Status: Retired 1995. Number: 24 . Thrust: 524.00 kN (117,799 lbf). Gross mass: 13,100 kg (28,800 lb). Unfuelled mass: 2,800 kg (6,100 lb). Specific impulse: 285 s. Specific impulse sea level: 220 s. Burn time: 70 s. Height: 6.19 m (20.30 ft). Diameter: 1.41 m (4.62 ft).

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.

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