This page no longer updated from 31 October 2001. Latest version can be found at S1.35800

Other Designations: S1.35800. Designer: Korolev. Developed in: 1954-57. Application: R-7 verniers. Propellants: Lox/Kerosene Thrust(vac): 3,100 kgf. Thrust(vac): 30.00 kN. Country: Russia. Status: Out of Production. Comments: Thrust variable 2.5-3.1 tf.
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Last update 12 March 2001.
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© Mark Wade, 2001 .