RD-0244-HC

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RD-0244-HC

Part of RD-0243

Kosberg LOx/Kerosene rocket engine. Design concept 1990's. Proposed variant of RD-0244 engine using LOX-kerosene instead of N2O4/UDMH as propellants.

AKA: RD-0244 KD. Status: Design concept 1990's. Thrust: 690.00 kN (155,110 lbf). Unfuelled mass: 540 kg (1,190 lb). Specific impulse: 332 s.

Engine: 540 kg (1,190 lb). Chamber Pressure: 230.00 bar. Thrust to Weight Ratio: 130.29. Oxidizer to Fuel Ratio: 2.7.

Country: Russia. Propellants: Lox/Kerosene. Agency: Kosberg bureau.

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