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M34
Nissan solid rocket engine. Used on M-V launch vehicle. First flight 1997. M-V third stage.

AKA: M-34;M-V-3. Status: Active. Number: 7 . Thrust: 294.20 kN (66,139 lbf). Gross mass: 11,000 kg (24,000 lb). Unfuelled mass: 1,000 kg (2,200 lb). Specific impulse: 301 s. Burn time: 102 s. Height: 3.60 m (11.80 ft). Diameter: 2.20 m (7.20 ft).

Chamber Pressure: 59.00 bar. Area Ratio: 96.



Country: Japan. Launch Vehicles: M-V, M-V KM. Propellants: Solid. Stages: M34. Agency: Nissan.

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