| Kartukov Soyuz SAS |
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Engine Model: Kartukov Soyuz SAS. Designer: Kartukov. Developed in: 1962-66. Application: Soyuz 7K-OK, Soyuz 7KT-OK, Soyuz 7K-T. Propellants: Solid. Thrust(vac): 785.000 kN (176,475 lbf). Country: Russia. Status: Out of Production. Thrust 76 tf at cutout - 80.1tf 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. |