This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Manufacturer Name: RD-0231. Designer: Kosberg. Developed in: 1968-70. Application: P-700 Granit. Used on spacecraft: Granat. Propellants: N2O4/UDMH Thrust(vac): 2,960 kgf. Thrust(vac): 29.00 kN. Isp: 275 sec. Burn time: 16 sec. Mass Engine: 28 kg. Diameter: 0.1 m. Length: 0.6 m. Chambers: 1. Chamber Pressure: 123.00 bar. Country: Russia. Status: Out of Production. First Flight: 1970. References: 307 . Comments: Staged combustion cycle.
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 .