XF 24B SkySlayer
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The XF 24B "SkySlayer" was an experimental aircraft designed by the USAF to test combat feasability and advantages of a reversed swept wing. 10 prototypes were made and were fitted with Air to Air and Air to Ground missles, alongside a 20mm minigun for test purposes.
Development: Developed under USAF Order Number 2310 by Lockheed Martin in 1999 through 2001. Each aircrafy cost around 50 million dollars each as they were fitted with extremely advanced systems.
Controls: Standard plane controls.
Note: All missles have Impact Cameras on.
Specifications
General Characteristics
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- Wingspan 25.6ft (7.8m)
- Length 44.3ft (13.5m)
- Height 11.4ft (3.5m)
- Empty Weight 9,924lbs (4,501kg)
- Loaded Weight 21,784lbs (9,881kg)
Performance
- Power/Weight Ratio 1.547
- Wing Loading 145.2lbs/ft2 (709.2kg/m2)
- Wing Area 150.0ft2 (13.9m2)
- Drag Points 2265
Parts
- Number of Parts 47
- Control Surfaces 8
- Performance Cost 364