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S5.44
Isayev Nitric acid/Amine rocket engine. SAM-missile 5Ya24. Out of Production. Could be throttled. 177-49 kN sea-level. Area ratio 118 - 44.

AKA: 5D25. Status: Out of Production. Date: 1964-65. Thrust: 177.00 kN (39,791 lbf). Unfuelled mass: 124 kg (273 lb). Specific impulse: 251 s. Specific impulse sea level: 251 s. Height: 1.71 m (5.62 ft). Diameter: 0.54 m (1.77 ft).

Throttled thrust(vac): 49.000 kN (11,015 lbf). Engine: 124 kg (273 lb). Area Ratio: 118. Propellant Formulation: AK27I/TG-02. Thrust to Weight Ratio: 145.16.



Family: Storable liquid. Country: Russia. Launch Vehicles: S-25. Propellants: Nitric acid/Amine. Agency: Isayev bureau. Bibliography: 320, 342.

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