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RD-0256-Methane
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Manufacturer Name: RD-0256-Methan. Designer: Kosberg. Developed in: 1996-. Propellants: Lox/LCH4. Thrust(vac): 836.000 kN (187,940 lbf). Isp: 353 sec. Mass Engine: 770 kg (1,690 lb). Chambers: 1. Chamber Pressure: 176.00 bar. Oxidizer to Fuel Ratio: 3.40. Thrust to Weight Ratio: 110.71. Country: Russia. Status: Design concept 1996-. Proposed variant of RD-0256 engine using LOX-liquid methane instead of N2O4/UDMH as propellants.
Bibliography and Further Reading - Russian Arms Catalogue, Vol 5 and 6, Military Parade, Moscow via Dietrich Haeseler.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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