F-16 Fighting Falcon
Crew: 1
Length: 49 ft 5 in (15.06 m)
Wingspan: 32 ft 8 in (9.96 m)
Height: 16 ft (4.9 m)
Wing area: 300 sq ft (28 m2)
Airfoil: NACA 64A204[259]
Empty weight: 18,900 lb (8,573 kg)
Gross weight: 26,500 lb (12,020 kg)
Max takeoff weight: 42,300 lb (19,187 kg)
Fuel capacity: 7,000 pounds (3,200 kg) internal[67]
Powerplant: 1 × General Electric F110-GE-129 for Block 50 aircraft , 17,155 lbf (76.31 kN) thrust dry, 29,500 lbf (131 kN) with afterburner
(1 × Pratt & Whitney F100-PW-229 for Block 52 aircraft, 17,800 lbf (79 kN) thrust dry and 29,160 lbf (129.7 kN) with afterburner.)
Performance
Maximum speed: Mach 2.05, 1,176 kn (1,353 mph; 2,178 km/h) at 40,000 feet, clean[76]
Mach 1.2, 800 kn (921 mph; 1,482 km/h) at sea level[76]
Combat range: 295 nmi (339 mi, 546 km) on a hi-lo-hi mission with 4 × 1,000 lb (454 kg) bombs
Ferry range: 2,277 nmi (2,620 mi, 4,217 km) with drop tanks
Service ceiling: 50,000 ft (15,000 m) [67]
g limits: +9.0
Roll rate: 324°/s[260]
Wing loading: 88.3 lb/sq ft (431 kg/m2)
Thrust/weight: 1.095 (1.24 with loaded weight & 50% internal fuel)[N 2]
Specifications
General Characteristics
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- Wingspan 33.6ft (10.3m)
- Length 56.2ft (17.1m)
- Height 18.2ft (5.5m)
- Empty Weight N/A
- Loaded Weight 30,898lbs (14,015kg)
Performance
- Power/Weight Ratio 4.363
- Wing Loading 44.4lbs/ft2 (216.7kg/m2)
- Wing Area 696.3ft2 (64.7m2)
- Drag Points 8016
Parts
- Number of Parts 720
- Control Surfaces 3
- Performance Cost 3,190
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