M-23-J

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M-23-J

Part of M-10

Nissan solid rocket engine. In development. Used on J-1 launch vehicle. First flight 1996. Solid propellant rocket stage. Version for J-1 F2 has 300 kg heavier empty mass. J-1 second stage.

AKA: J-1-2. Status: In development. Number: 1 . Thrust: 524.80 kN (117,980 lbf). Gross mass: 12,800 kg (28,200 lb). Unfuelled mass: 2,400 kg (5,200 lb). Specific impulse: 282 s. Burn time: 73 s. Height: 2.70 m (8.80 ft). Diameter: 1.40 m (4.50 ft).

Area Ratio: 23.

Country: Japan. Launch Vehicles: J-1, J-1 F2. Propellants: Solid. Stages: M-23-J. Agency: Nissan.

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