This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Kartukov Soyuz T - TM SAS 17k


Designer: Kartukov. Developed in: -1979. Application: Soyuz T, Soyuz TM. Used on spacecraft: Soyuz T, Soyuz TM. Propellants: Solid Thrust(vac): 17,500 kgf. Thrust(vac): 171.00 kN. Country: Russia. Status: In Production. Comments: Thrust 10 tf at cutout - 17.5 at ignition.
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 .