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RD-0245-HC
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Manufacturer Name: RD-0245-HC. Designer: Kosberg. Propellants: Lox/Kerosene. Thrust(vac): 214.000 kN (48,109 lbf). Isp: 320 sec. Mass Engine: 290 kg (630 lb). Chambers: 4. Chamber Pressure: 142.00 bar. Oxidizer to Fuel Ratio: 2.30. Thrust to Weight Ratio: 75.24. Country: Russia. Status: Design concept 1990's. Proposed variant of RD-0245 engine using LOX-kerosene 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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