F-16 Falcon - The Technology

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June 26, 2020

F-16 Falcon

F-16, also called Fighting Falcon, single-seat, single-engine, supersonic, multirole jet fighter built by the General Dynamics Corporation (now part of the Lockheed Martin Corporation) for the United States and more than a dozen other countries. Over 4,600 aircraft have been built since production was approved in 1976. 


The Fighting Falcon's key features include a frameless bubble canopy for better visibility, side-mounted control stick to ease control while maneuvering, an ejection seat reclined 30 degrees from vertical to reduce the effect of g-forces on the pilot, and the first use of a relaxed static stability/fly-by-wire flight control system which helps to make it an agile aircraft.



Aircraft Specifications

Length

49.3 ft / 15.027 m

Height

16.7 ft / 5.090 m

Wingspan

31.0 ft / 9.449 m 

Wing Area

27.87 sq. m (300 sq. ft)

Aspect Ratio

3.2

Empty weight

20,300 lb / 9,207 kg 

Max. Take-off Weight

48,000 lb / 21,772 kg 

Fuel capacity

7,000 pounds (3,200 kg) internals

Engine/Powerplant

PW F100-PW-200 (23,800 lbf (106 kN)) or GE F110-GE-100 (28,600 lbf (127 kN) or GE F110-GE-132 (32,500 lbf (145 kN))

Number of Engines

1

Thrust to weight ratio

1.096

Wing Loading

688.9 kg/sq. m 

141.1 lb/sq. ft

Aircraft performance

Max speed

1,500 mph (Mach 2 at altitude)

Range 

Over 2,100 nm (2,425 mi; 3,900 km)

Service ceiling

Above 50,000 feet (15 kilometers)

G limit 

9

Rate of climb 

+50,000 ft/min (250 m/s)

Cruise speed

577 mph (929 kmph)


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