Engine Model: F100-100. Designer: Pratt and Whitney. Propellants: Air/Kerosene. Thrust(vac): 63.900 kN (14,365 lbf). Thrust(sl): 58.100 kN (13,061 lbf). Isp: 1,552 sec. Burn time: 7,000 sec. Chambers: 1. Country: USA. Status: In Production. Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust.
F100 used on Rocket Stages