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Engine Model: RD-200. Manufacturer Name: RD-200. Designer: Glushko. Developed in: -1951. Application: vertical sounding rocket. Propellants: Nitric acid/Kerosene. Thrust(vac): 98.508 kN (22,145 lbf). Isp: 234 sec. Isp (sea level): 210 sec. Burn time: 605 sec. Mass Engine: 218 kg (480 lb). Diameter: 0.53 m (1.73 ft). Length: 0.51 m (1.66 ft). Chamber Pressure: 23.50 bar. Area Ratio: 4.00. Oxidizer to Fuel Ratio: 3.76. Thrust to Weight Ratio: 46.07. Country: Russia. Status: Developed -1951.
Bibliography:- Glushko, V P, Albom Konstruktsiy ZhRD, Vol. 1 1968, Vol. 3 & 4 1969 via Dietrich Haeseler.
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