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RKDS-100
Glushko LOx/Kerosene rocket engine. Keldysh Bomber. Design 1946. Nominal design engine for 1946 Keldysh bomber design. The Soviet Union would not produce an engine with these propellants and thrust levels until nearly 20 years later.

Status: Design 1946. Date: 1946. Thrust: 980.00 kN (220,310 lbf). Unfuelled mass: 2,500 kg (5,500 lb). Specific impulse: 285 s. Specific impulse sea level: 252 s. Burn time: 200 s. Diameter: 1.12 m (3.69 ft).

Engine: 2,500 kg (5,500 lb). Chamber Pressure: 40.00 bar. Area Ratio: 6.58. Thrust to Weight Ratio: 40.



Country: Russia. Launch Vehicles: Keldysh Bomber. Propellants: Lox/Kerosene. Stages: Keldysh Bomber stage, Keldysh Sled. Agency: Glushko bureau.

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