Northrop F-20 Tigershark
he Northrop F-20 Tigershark (initially F-5G) was a privately financed light fighter, designed and built by Northrop. Its development began in 1975 as a further evolution of Northrop's F-5E Tiger II, featuring a new engine that greatly improved overall performance, and a modern avionics suite including a powerful and flexible radar. Compared with the F-5E, the F-20 was much faster, gained beyond-visual-range air-to-air capability, and had a full suite of air-to-ground modes capable of firing most U.S. weapons. With these improved capabilities, the F-20 became competitive with contemporary fighter designs such as the General Dynamics F-16 Fighting Falcon, but was much less expensive to purchase and operate. PRESS 1 TO JETTISON FUEL TANKS.
Specifications
General Characteristics
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- Wingspan 23.9ft (7.3m)
- Length 37.0ft (11.3m)
- Height 12.3ft (3.7m)
- Empty Weight 9,218lbs (4,181kg)
- Loaded Weight 11,840lbs (5,370kg)
Performance
- Power/Weight Ratio 2.846
- Wing Loading 38.7lbs/ft2 (189.0kg/m2)
- Wing Area 306.0ft2 (28.4m2)
- Drag Points 3379
Parts
- Number of Parts 55
- Control Surfaces 5
- Performance Cost 325