Specifications
| Type | single-seat fighter aircraft |
| Contractor | General Dynamics |
| Country of Origin | USA |
| Powerplant | one General Electric F110-GE-100 or one Pratt & Whitney F100-P-220 turbofan engines |
| Thrust | 27,600lbs reheated (General Electric) 23,450lbs reheated (Pratt & Whitney) |
| Length | 49ft 5in |
| Height | 16ft 8.5in |
| Wingspan | 32ft 10in |
| Wing Area | 300 Sq. ft |
| Max Speed | 1,320mph (mach 2+) @ 40,000ft |
| Climb Rate | 50,000ft/minute |
| Service Ceiling | 50,000+ft |
| Radius | 575+ miles |
| Empty Weight | 18,335lbs |
| Max Take-Off Weight | 42,300lbs |
| Armament | Mk 82, and 84 bombs AGM 65, and 88 air-to-ground missiles CBU 87, 89, 97 cluster bombs GBU 10, and 12 guided bombs AIM-9 Sidewinder air-to-air missiles AIM-120 AMRAAM air-to-air missiles |