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RD-0231
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Manufacturer Name: RD-0231. Designer: Kosberg. Developed in: 1968-70. Application: P-700 Granit. Propellants: N2O4/UDMH. Thrust(vac): 29.000 kN (6,519 lbf). Isp: 275 sec. Burn time: 16 sec. Mass Engine: 28 kg (61 lb). Diameter: 0.15 m (0.49 ft). Length: 0.60 m (1.96 ft). Chambers: 1. Chamber Pressure: 123.00 bar. Thrust to Weight Ratio: 105.71. Country: Russia. Status: Out of Production. First Flight: 1970. Staged combustion cycle.
RD-0231 used on Spacecraft
Bibliography and Further Reading - Haeseler, Dietrich, Visit to the museum of Chemical Automatics Design Bureau, Voronezh 1992 via Dietrich Haeseler.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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