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S2.720
Isayev Nitric acid/Amine rocket engine. Engine for SAM-missile V-755. Out of Production. Pump-fed engine. Used in engine unit of a special apparatus. Pump-fed engine. 20,4 kN sea level.

Status: Out of Production. Thrust: 34.30 kN (7,711 lbf). Unfuelled mass: 48 kg (105 lb). Specific impulse: 233 s. Specific impulse sea level: 233 s. Burn time: 55 s. Height: 0.95 m (3.10 ft). Diameter: 0.48 m (1.56 ft).

Thrust (sl): 34.300 kN (7,711 lbf). Thrust (sl): 3,500 kgf. Engine: 48 kg (105 lb). Chamber Pressure: 64.00 bar. Propellant Formulation: AK20K/TG-02. Thrust to Weight Ratio: 73.64. Oxidizer to Fuel Ratio: 3.23.



Family: Storable liquid. Country: Russia. Propellants: Nitric acid/Amine. Agency: Isayev bureau. Bibliography: 225, 329, 340, 342.

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