RD-2

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RD-2

Part of RD-1

Glushko Nitric acid/Kerosene rocket engine. experimental. Developed 1945-47. The RD-2 was based on the RD-1 engine. Used chemical ignition.

Status: Developed 1945-47. Date: 1945-47. Thrust: 6.00 kN (1,349 lbf). Unfuelled mass: 71 kg (156 lb). Specific impulse: 200 s.

Throttled thrust(vac): 2.000 kN (450 lbf). Engine: 71 kg (156 lb). Chamber Pressure: 20.60 bar. Thrust to Weight Ratio: 8.61.

Family: Storable liquid. Country: Russia. Propellants: Nitric acid/Kerosene. Agency: Glushko bureau. Bibliography: 342.

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