R-101B.36000-0

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R-101B.36000-0

Part of RD-0200

Isayev Nitric acid/Amine rocket engine. Single chamber engine designed for use in the R-101B and R-108 (derivative of German Wasserfall).

Status: Developed 1950-51. Date: July 1950. Thrust: 83.30 kN (18,727 lbf).

Never flown in this application but developed for use in the V-300 SAM and R-11 SSM.

Thrust (sl): 83.300 kN (18,727 lbf). Thrust (sl): 8,500 kgf. Propellant Formulation: AK20K/TG-02.

Family: Storable liquid. Country: Russia. Launch Vehicles: R-101, R-108. Propellants: Nitric acid/Amine. Agency: Isayev bureau.

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