| Navaho X-10 |
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Model: Navaho X-10. Gross Mass: 19,183 kg (42,291 lb). Empty Mass: 11,700 kg (25,700 lb). Thrust (vac): 96.948 kN (21,795 lbf). Isp: 1,800 sec. Burn time: 2,000 sec. Propellants: Air/Kerosene. Isp(sl): 1,800 sec. Diameter: 1.71 m (5.61 ft). Span: 8.59 m (28.18 ft). Length: 20.18 m (66.20 ft). Country: USA. No Engines: 2. Motor: XJ40-WE-1. Status: Out of production. Cost $ : 10.000 million. First Flight: 1950. Last Flight: 1959. No Launched: 37. Aerodynamic test vehicle for Navaho missile; Max speed Mach 2.08; range 1320 km. Used on Launch Vehicles: Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |