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 - 2007 except where otherwise noted.

 
Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z