J75-17
Designer: Pratt and Whitney. Propellants: Air/Kerosene. Thrust(vac): 71.600 kN (16,096 lbf). Thrust(sl): 65.100 kN (14,635 lbf). Isp: 1,800 sec. Burn time: 6,000 sec. Chambers: 1. Country: USA. Status: Out of Production.

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

J75-17 used on Rocket Stages

 
 
 
 
 
 
 
 
 
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