M-30 (original) (raw)

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M-30

Nissan solid rocket engine. Mu-3D third stage.

AKA: Mu-3D-3. Status: Retired 1972. Thrust: 128.00 kN (28,775 lbf). Gross mass: 2,800 kg (6,100 lb). Unfuelled mass: 773 kg (1,704 lb). Burn time: 42 s. Height: 4.00 m (13.10 ft). Diameter: 0.86 m (2.82 ft).

Country: Japan. Launch Vehicles: Mu-1, Mu-3D, Mu-4S. Propellants: Solid. Stages: M-30. Agency: Nissan.

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