| Kartukov Soyuz T - TM SAS 73k |
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Engine Model: Kartukov Soyuz T - TM SAS 73k. Designer: Kartukov. Developed in: -1979. Application: Soyuz T, Soyuz TM. Propellants: Solid. Thrust(vac): 715.000 kN (160,738 lbf). Country: Russia. Status: In Production. Thrust 45 tf at cutout - 73 tf at ignition. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |