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Manufacturer Name: RD-200. Designer: Glushko. Developed in: -1951. Application: vertical sounding rocket. Propellants: Nitric acid/Kerosene Thrust(vac): 10,045 kgf. Thrust(vac): 98.51 kN. Isp: 234 sec. Isp (sea level): 210 sec. Burn time: 605 sec. Mass Engine: 218 kg. Diameter: 0.5 m. Length: 0.5 m. Chamber Pressure: 23.50 bar. Area Ratio: 4.00. Oxidizer to Fuel Ratio: 3.76. Country: Russia. Status: Developed -1951. References: 320 .
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Last update 12 March 2001.
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