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RD-0242M1
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Manufacturer Name: RD-0242M1. Designer: Kosberg. Developed in: 1998-. Propellants: N2O4/MMH. Thrust(vac): 98.100 kN (22,054 lbf). Isp: 343 sec. Burn time: 600 sec. Mass Engine: 229 kg (504 lb). Diameter: 1.25 m (4.10 ft). Length: 2.34 m (7.67 ft). Chambers: 1. Chamber Pressure: 153.00 bar. Thrust to Weight Ratio: 43.68. Country: Russia. Status: Design concept 1998-. Proposed variant of RD-0242 engine for upper stages using MMH in place of UDMH (adaptation to western market ?). Reusable for 6 ignitions total. Throttling to 80%.
Bibliography and Further Reading - Haeseler, Dietrich, CADB-information leaflets, International Aerospace Show Berlin 1998 (ILA 98) via Dietrich Haeseler.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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