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.
Status: Developed 1941-46. Date: 1941-46. Thrust: 2.94 kN (661 lbf). Unfuelled mass: 60 kg (132 lb). Specific impulse: 200 s.
Engine: 60 kg (132 lb). Chamber Pressure: 22.00 bar. Thrust to Weight Ratio: 5.