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M-3A
Part of M-3 Family
Nissan solid rocket engine.

Status: Retired 1984. Thrust: 61.00 kN (13,713 lbf). Gross mass: 1,100 kg (2,400 lb). Unfuelled mass: 130 kg (280 lb). Burn time: 54 s. Height: 2.30 m (7.50 ft). Diameter: 1.14 m (3.74 ft).



Country: Japan. Launch Vehicles: Mu-3C, Mu-3H, Mu-3S. Propellants: Solid. Stages: M-3A. Agency: Nissan.

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