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RD-0234-HC
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Manufacturer Name: RD-0234-HC. Designer: Kosberg. Developed in: 1996-. Propellants: Lox/Kerosene. Thrust(vac): 516.000 kN (116,001 lbf). Isp: 331 sec. Isp (sea level): 310 sec. Mass Engine: 390 kg (850 lb). Chambers: 1. Chamber Pressure: 196.00 bar. Oxidizer to Fuel Ratio: 2.60. Thrust to Weight Ratio: 134.91. Country: Russia. Status: Developed 1996-. Proposed variant of RD-0234 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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