JP-5/H2O2
Propellants: H2O2/Kerosene. Thrust(vac): 63.000 kN (14,162 lbf). Isp: 335 sec. Burn time: 560 sec. Chambers: 1. Country: USA. Status: Study 1993.

Selected propellants for Black Horse winged, single stage to orbit launch vehicle using aerial refueling and lower performance, non-cryogenic propellants. Takes off from runway at 48,452 lbs gross weight; rendezvous with tanker to load 146,870 lbs oxidizer; then flies to orbit.

JP-5/H2O2 used on Rocket Stages

 
 
 
 
 
 
 
 
 
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