Status: Developed 1941-45. Date: 1941-45. Thrust: 2.94 kN (661 lbf). Unfuelled mass: 56 kg (123 lb). Specific impulse: 200 s.
Engine: 56 kg (123 lb). Chamber Pressure: 20.00 bar. Thrust to Weight Ratio: 5.35.
RD-1KhZ Glushko Nitric acid/Kerosene rocket engine. take-off acceleration of Pe-2R, La-7R, Yak-3, Su-6, Su-7, La-120R airplanes. Developed 1941-46. The RD-1KhZ was a variant of the RD-1 engine with chemical ignition. Production 1944-45.RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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