This page no longer updated from 31 October 2001. Latest version can be found at 11D23

Designer: Kosberg. Used on spacecraft: LK-700. Propellants: N2O4/UDMH Thrust(vac): 23,500 kgf. Thrust(vac): 230.50 kN. Chambers: 1. Country: USSR. Status: Study 1968. References: 443 . Comments: Engine used in Block 1 and Block 11 stages of LK-700 manned lunar lander.
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 .