S1.35800 home
topic index
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.