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S09.502
Isayev Nitric acid/Amine rocket engine. Four chamber engine designed for use in the R-101 (derivative of German Wasserfall). Abandoned by 1950 in favor of single-chamber engine.

AKA: S9.502. Status: Developed 1949-50. Date: May 1949. Thrust: 78.40 kN (17,625 lbf).

Chambers: 4. Thrust (sl): 78.400 kN (17,625 lbf). Thrust (sl): 8,000 kgf. Propellant Formulation: AK20K/TG-02.

Family: Storable liquid. Country: Russia. Launch Vehicles: R-101. Propellants: Nitric acid/Amine. Agency: Isayev bureau.
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