Engine Model: 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