F-20A Tigershark: Difference between revisions
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{{Infobox Aircraft | {{Infobox Aircraft | ||
|name = | |name = F-20A Tigershark | ||
|Type = Fighter Aircraft | |Type = Fighter Aircraft | ||
|manufacture = Stone Oceanian Aero Tech | |manufacture = Stone Oceanian Aero Tech | ||
| Line 19: | Line 19: | ||
==Operators== | ==Operators== | ||
==Spectifications ( | ==Spectifications (F-20A Tigershark}== | ||
General characteristics | General characteristics | ||
Latest revision as of 08:36, 7 June 2023
| F-20A Tigershark | |
|---|---|
 | |
| History | |
| Manufactured | 1997-2015 |
Design
Operators
Spectifications (F-20A Tigershark}
General characteristics
Crew: 1 Length: 47 ft 4 in (14.43 m) Wingspan: 27 ft 11.875 in (8.53123 m) with wing-tip missiles 26 ft 8 in (8.13 m) clean Height: 13 ft 10.25 in (4.2228 m) Empty weight: 11,810 lb (5,357 kg) Gross weight: 16,015 lb (7,264 kg) Combat TOW - 50% fuel 2x AIM-9 Max takeoff weight: 27,500 lb (12,474 kg) Fuel capacity: 5,050 lb (2,291 kg) in integral and bladder tanks Powerplant: 1 × General Electric F404-GE-100 afterburning turbofan engine, 11,000 lbf (49 kN) thrust dry, 17,000 lbf (76 kN) with afterburner