Encyclopedia entry

RD-200

Engine · Russia

Original archive entry. The text, images and links below are kept as they were written.

Glushko Nitric acid/Kerosene rocket engine. vertical sounding rocket. Developed -1951.

Engine: 218 kg (480 lb). Chamber Pressure: 23.50 bar. Area Ratio: 4. Propellant Formulation: HNO3/TM-114. Thrust to Weight Ratio: 46.07. Oxidizer to Fuel Ratio: 3.76.

Family: Storable liquid
Country: Russia
Propellants: Nitric acid/Kerosene
Agency: Glushko bureau
Bibliography: 320

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