Auto Credit Based on DALS's F-16 Fighting Falcon (Unarmed)
In 1993 Lockheed Martin proposed development of a new version of the venerable F-16.
This F-16X 'Falcon 2000' featured a delta-wing planform like that of the F-22; together with the fuselage stretch to accommodate the new wing design, the F-16X would have 80% more internal fuel volume.
The design also permitted conformal carriage of the AIM-120 AMRAAM. LM claimed the F-16X could be built for two-thirds the cost of the F/A-18E/F Super Hornet.
Another great variant of my F-16s Enjoy, Upvote and Comment.
Information from Wikipedia source: https://en.wikipedia.org/wiki/General_Dynamics_F-16_Fighting_Falcon_variants#F-16X_Falcon_2000
Specifications
General Characteristics
- Predecessor F-16 Fighting Falcon (Unarmed)
- Created On Windows
- Wingspan 26.0ft (7.9m)
- Length 36.6ft (11.1m)
- Height 12.0ft (3.7m)
- Empty Weight 6,657lbs (3,019kg)
- Loaded Weight 13,206lbs (5,990kg)
Performance
- Power/Weight Ratio 2.552
- Wing Loading 38.8lbs/ft2 (189.7kg/m2)
- Wing Area 340.0ft2 (31.6m2)
- Drag Points 1929
Parts
- Number of Parts 53
- Control Surfaces 8
- Performance Cost 305
