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M24
Part of M14 Family
Nissan solid rocket engine. Used on M-V launch vehicle. First flight 1997. M-V second stage.

AKA: M-24;M-V-2. Status: Active. Number: 7 . Thrust: 1,245.30 kN (279,955 lbf). Gross mass: 34,470 kg (75,990 lb). Unfuelled mass: 3,410 kg (7,510 lb). Specific impulse: 288 s. Specific impulse sea level: 203 s. Burn time: 71 s. Height: 6.80 m (22.30 ft). Diameter: 2.50 m (8.20 ft).

Thrust (sl): 877.700 kN (197,315 lbf). Thrust (sl): 89,506 kgf. Chamber Pressure: 59.00 bar. Area Ratio: 31.



Country: Japan. Launch Vehicles: M-V, M-V KM. Propellants: Solid. Stages: M24. Agency: Nissan.

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