This page no longer updated from 31 October 2001. Latest version can be found at 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.
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Last update 12 March 2001.
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© Mark Wade, 2001 .