Black Horse
Black Horse

Credit - © Mark Wade
Gross Mass: 83,560 kg (184,210 lb). Empty Mass: 6,883 kg (15,174 lb). Thrust (vac): 443.191 kN (99,633 lbf). Isp: 335 sec. Burn time: 560 sec. Propellants: H2O2/Kerosene. Diameter: 6.30 m (20.60 ft). Span: 39.50 m (129.50 ft). Length: 57.50 m (188.60 ft). Country: USA. No Engines: 7. Engine: JP-5/H2O2. Status: Study 1993. Release conditions: 800 kph at 8.5 km.

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.


Used on Launch Vehicles:  
 
 
 
 
 
 
 
 

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© Mark Wade, 1997 - 2007 except where otherwise noted.

 
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