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Manufacturer Name: RD-0244-HC. Designer: Kosberg. Propellants: Lox/Kerosene Thrust(vac): 70,360 kgf. Thrust(vac): 690.00 kN. Isp: 332 sec. Mass Engine: 540 kg. Chambers: 1. Chamber Pressure: 230.00 bar. Oxidizer to Fuel Ratio: 2.70. Country: Russia. Status: Design concept 1990's. References: 342 . Comments: Proposed variant of RD-0244 engine using LOX-kerosene instead of N2O4/UDMH as propellants.
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Last update 12 March 2001.
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