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The F-16's key features include a frameless bubble canopy for enhanced cockpit visibility, a 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 that helps ...
Autonomous air combat maneuvering instrumentation (AACMI) are second-generation GPS-based ACMI systems.. Unlike first-generation ACMI systems, which use ground radars to track and record the position of the aircraft on the range, AACMI systems use aircraft-mounted satellite navigation systems such as the US NAVSTAR GPS system.
F-16 simulator side-stick controller functional allocation (for the right hand) F-16 simulator throttle functional allocation (for the left hand). HOTAS, an acronym of hands on throttle-and-stick, is the concept of placing buttons and switches on the throttle lever and flight control stick in an aircraft cockpit.
The side-stick is used in many modern military fighter aircraft, such as the F-16 Fighting Falcon, Mitsubishi F-2, Dassault Rafale, and F-22 Raptor, F-35 Lightning 2, Chengdu J-20, AIDC F-CK 1 Ching-Kuo and also on civil aircraft, such as the Sukhoi Superjet 100, Airbus A320 and all subsequent Airbus aircraft, [2] including the largest passenger jet in service, the Airbus A380.
The AN/APG-68 radar is a long range (Max Detection Range 80 kilometres [50 mi]) [2] Pulse-Doppler radar designed by Westinghouse (now Northrop Grumman) to replace AN/APG-66 radar in the General Dynamics F-16 Fighting Falcon. The AN/APG-68 radar is now currently being replaced on US Air Force F-16C/D Block 40/42 and 50/52 by the AN/APG-83 AESA ...
Footage and photos show the Su-35 flying past the F-16 during an intercept of a Russian aircraft. A Russian military jet flew dangerously close to a US aircraft during an intercept near Alaska ...
Turkey has reduced its planned $23 billion acquisition of an F-16 fighter jet package from the United States, scrapping the purchase of 79 modernisation kits for its existing fleet, Defence ...
Data from USAF fact sheet AerospaceWeb General characteristics Crew: 2 (pilot and safety pilot) Length: 48 ft 7 in (14.8 m) Wingspan: 32 ft 2 in (9.8 m) Height: 15 ft 9 in (4.8 m) Wing area: 300 sq ft (28 m 2) Airfoil: NACA 64A204 root and tip Empty weight: 18,238 lb (8,273 kg) Gross weight: 26,463 lb (12,003 kg) Max takeoff weight: 42,300 lb (19,187 kg) Powerplant: 1 × General Electric F110 ...