J93-3
Designer: General Electric. Propellants: Air/Kerosene. Thrust(vac): 86.700 kN (19,491 lbf). Thrust(sl): 78.800 kN (17,715 lbf). Isp: 2,084 sec. Burn time: 11,000 sec. Chambers: 1. Country: USA. Status: Out of Production.

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

J93-3 used on Rocket Stages

 
 
 
 
 
 
 
 
 
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