Black Horse AV
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: © Mark Wade
H2O2/Kerosene propellant rocket stage. 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.
No Engines: 7. Release conditions: 800 kph at 8.5 km.
Related
- Country
- USA
- Engines
- JP-5/H2O2
- Launch Vehicles
- Black Horse
- Propellants
- H2O2/Kerosene