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RD-210
Glushko Nitric acid/Kerosene rocket engine. vertical sounding rocket. Developed -1954.

Status: Developed -1954. Date: -1954. Thrust: 29.85 kN (6,711 lbf). Unfuelled mass: 81 kg (178 lb). Specific impulse: 241 s. Specific impulse sea level: 214 s. Burn time: 60 s. Height: 1.40 m (4.50 ft). Diameter: 0.40 m (1.31 ft).

Engine: 81 kg (178 lb). Chamber Pressure: 23.50 bar. Area Ratio: 4.16. Propellant Formulation: HNO3/TM-114. Thrust to Weight Ratio: 37.76. Oxidizer to Fuel Ratio: 4.12.



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

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