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M-13
Part of M-10 Family
Nissan solid rocket engine. Used on Mu-3S launch vehicle. First flight 1969.

AKA: M-13TVC; Mu-3S-1. Status: Retired 1995. Number: 24 . Thrust: 1,262.40 kN (283,799 lbf). Gross mass: 34,800 kg (76,700 lb). Unfuelled mass: 7,640 kg (16,840 lb). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 70 s. Height: 14.75 m (48.39 ft). Diameter: 1.41 m (4.62 ft).

Thrust (sl): 1,142.400 kN (256,822 lbf). Thrust (sl): 116,494 kgf.

Country: Japan. Launch Vehicles: Mu-3H, Mu-3S, Mu-3S-II. Propellants: Solid. Stages: M-13. Agency: Nissan. More at: 9678.



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