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RD-0210-HC
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Manufacturer Name: RD-0210-HC. Designer: Kosberg. Propellants: Lox/Kerosene. Thrust(vac): 592.000 kN (133,086 lbf). Isp: 342 sec. Mass Engine: 570 kg (1,250 lb). Chambers: 1. Chamber Pressure: 147.00 bar. Oxidizer to Fuel Ratio: 2.60. Thrust to Weight Ratio: 105.90. Country: Russia. Status: Design concept 1990's. Proposed variant of RD-0210 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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