F101
Designer: Pratt and Whitney. Propellants: Air/Kerosene. Thrust(vac): 75.600 kN (16,996 lbf). Thrust(sl): 68.700 kN (15,444 lbf). Isp: 1,980 sec. Burn time: 33,000 sec. Chambers: 1. Country: USA. Status: In Production.

Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust.

F101 used on Rocket Stages

  • Used on stage: B-1A.
 
 
 
 
 
 
 
 
 
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