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Engine Model: RD-210. Manufacturer Name: RD-210. Designer: Glushko. Developed in: -1954. Application: vertical sounding rocket. Propellants: Nitric acid/Kerosene. Thrust(vac): 29.850 kN (6,711 lbf). Isp: 241 sec. Isp (sea level): 214 sec. Burn time: 60 sec. Mass Engine: 81 kg (178 lb). Diameter: 0.40 m (1.31 ft). Length: 1.40 m (4.50 ft). Chamber Pressure: 23.50 bar. Area Ratio: 4.16. Oxidizer to Fuel Ratio: 4.12. Thrust to Weight Ratio: 37.76. Country: Russia. Status: Developed -1954.
Bibliography:- Glushko, V P, Albom Konstruktsiy ZhRD, Vol. 1 1968, Vol. 3 & 4 1969 via Dietrich Haeseler.
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