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astronautix.com RD-0245-HC


Manufacturer Name: RD-0245-HC. Designer: Kosberg. Propellants: Lox/Kerosene Thrust(vac): 21,822 kgf. Thrust(vac): 214.00 kN. Isp: 320 sec. Mass Engine: 290 kg. Chambers: 4. Chamber Pressure: 142.00 bar. Oxidizer to Fuel Ratio: 2.30. Country: Russia. Status: Design concept 1990's. References: 342 . Comments: Proposed variant of RD-0245 engine using LOX-kerosene instead of N2O4/UDMH as propellants.
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Last update 12 March 2001.
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