This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Glushko. Developed in: 1946. Application: Keldysh Bomber. Used on stages: Keldysh Sled, Keldysh Bomber. Used on launch vehicles: Keldysh Bomber. Propellants: Lox/Kerosene Thrust(vac): 100,000 kgf. Isp: 285 sec. Isp (sea level): 252 sec. Burn time: 200 sec. Mass Engine: 2,500 kg. Diameter: 1.1 m. Chambers: 1. Chamber Pressure: 40.00 bar. Area Ratio: 6.58. Thrust to Weight Ratio: 40.00. Country: USSR. Status: Study 1946. Comments: 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.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .