This page no longer updated from 31 October 2001. Latest version can be found at RD-0231

Manufacturer Name: RD-0231. Designer: Kosberg. Developed in: 1968-70. Application: P-700 Granit. Used on spacecraft: Granat. Propellants: N2O4/UDMH Thrust(vac): 2,960 kgf. Thrust(vac): 29.00 kN. Isp: 275 sec. Burn time: 16 sec. Mass Engine: 28 kg. Diameter: 0.1 m. Length: 0.6 m. Chambers: 1. Chamber Pressure: 123.00 bar. Country: Russia. Status: Out of Production. First Flight: 1970. References: 307 . Comments: Staged combustion cycle.
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Last update 12 March 2001.
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© Mark Wade, 2001 .