M-3B-J

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M-3B-J

Part of M-3B-Mu

Nissan solid rocket engine. In development. Used on J-1 launch vehicle. First flight 1996.

AKA: M-3B. Status: In development. Number: 1 . Thrust: 132.10 kN (29,697 lbf). Gross mass: 3,600 kg (7,900 lb). Unfuelled mass: 300 kg (660 lb). Specific impulse: 294 s. Burn time: 87 s. Height: 2.70 m (8.80 ft). Diameter: 1.50 m (4.90 ft).

Area Ratio: 52.

Country: Japan. Launch Vehicles: J-1. Propellants: Solid. Stages: M-3B-Mu. Agency: Nissan.

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