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RD-200
Glushko Nitric acid/Kerosene rocket engine. vertical sounding rocket. Developed -1951.

Status: Developed -1951. Date: -1951. Thrust: 98.51 kN (22,145 lbf). Unfuelled mass: 218 kg (480 lb). Specific impulse: 234 s. Specific impulse sea level: 210 s. Burn time: 605 s. Height: 0.51 m (1.66 ft). Diameter: 0.53 m (1.73 ft).

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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