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Navaho development
Navaho development sequenceCredit: © Mark Wade. 7,273 bytes. 614 x 366 pixels. |
Family: Navaho. Country: USA. Status: Hardware. Department of Defence Designation: X-10.
Aerodynamic test vehicle for Navaho missile; Max speed Mach 2.08; range 1320 km.
SpecificationsLiftoff Thrust: 9,890 kgf. Total Mass: 19,183 kg. Core Diameter: 1.7 m. Total Length: 24.0 m. Flyaway Unit Cost $: 10.00 million. in 1985 unit dollars.
- Stage Number: 1. 1 x Navaho X-10 Gross Mass: 19,183 kg. Empty Mass: 11,700 kg. Thrust (vac): 9,886 kgf. Isp: 1,800 sec. Burn time: 2,000 sec. Isp(sl): 1,800 sec. Diameter: 1.7 m. Span: 8.6 m. Length: 20.2 m. Propellants: Air/Kerosene No Engines: 2. XJ40-WE-1
Bibliography:- 48 - Miller, Jay,, The X-Planes, Aerofax, Arlington, Texas, 1988.
- 221 - Gibson, James N, The Navaho Missile Project, Schiffer, 1996.
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Last update 12 March 2001.
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