| S1.35800 |
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Engine Model: S1.35800. Other Designations: S1.35800. Designer: Korolev. Developed in: 1954-57. Application: R-7 verniers. Propellants: Lox/Kerosene. Thrust(vac): 30.000 kN (6,744 lbf). Country: Russia. Status: Out of Production. Thrust variable 2.5-3.1 tf 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. |