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S5.3M
Part of S5.3
Isayev Nitric acid/Amine rocket engine. R-9 (SS-8) missile stage 1. Out of Production. Proposed for R-9 missile stage 1. Four engines per stage. 396,7 kN sea-level.

Status: Out of Production. Date: 1959-60, 1958-60. Thrust: 396.70 kN (89,182 lbf). Unfuelled mass: 433 kg (954 lb). Specific impulse: 241 s. Specific impulse sea level: 241 s.

Chambers: 4. Engine: 433 kg (954 lb). Chamber Pressure: 66.00 bar. Area Ratio: 9.55. Propellant Formulation: AK27I/TG-02. Thrust to Weight Ratio: 93.42. Oxidizer to Fuel Ratio: 3.6.

Family: Storable liquid. Country: Russia. Launch Vehicles: 8K76, R-9A. Propellants: Nitric acid/Amine. Agency: Isayev bureau.
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