This page no longer updated from 31 October 2001. Latest version can be found at RD-210

Manufacturer Name: RD-210. Designer: Glushko. Developed in: -1954. Application: vertical sounding rocket. Propellants: Nitric acid/Kerosene Thrust(vac): 3,044 kgf. Thrust(vac): 29.85 kN. Isp: 241 sec. Isp (sea level): 214 sec. Burn time: 60 sec. Mass Engine: 81 kg. Diameter: 0.4 m. Length: 1.4 m. Chamber Pressure: 23.50 bar. Area Ratio: 4.16. Oxidizer to Fuel Ratio: 4.12. Country: Russia. Status: Developed -1954. References: 320 .
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Last update 12 March 2001.
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© Mark Wade, 2001 .