JP-5/H2O2

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JP-5/H2O2

Notional H2O2/Kerosene rocket engine. Study 1993. Engine for Black Horse winged, single stage to orbit launch vehicle using aerial refueling.

Status: Study 1993. Thrust: 63.00 kN (14,162 lbf). Specific impulse: 335 s. Burn time: 560 s.

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.

Propellant Formulation: H2O2/JP-5.

Family: Storable liquid. Country: USA. Launch Vehicles: Black Horse. Propellants: H2O2/Kerosene. Stages: Black Horse AV.

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