5 mlbf RP-4
Propellants: Lox/Kerosene. Thrust(vac): 24,459.000 kN (5,498,601 lbf). Isp: 299 sec. Isp (sea level): 260 sec. Burn time: 118 sec. Chambers: 1. Country: USA. Status: Study 1963. First Flight: 1977.

Operational date would have been July 1977. Recoverable stage. 10% plug nozzle.

5 mlbf RP-4 used on Rocket Stages

 
 
 
 
 
 
 
 
 
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