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The F-16 is a single-engine, highly maneuverable, supersonic, multirole tactical fighter aircraft. It is much smaller and lighter than its predecessors but uses advanced aerodynamics and avionics, including the first use of a relaxed static stability/fly-by-wire (RSS/FBW) flight control system, to achieve enhanced maneuver performance.
The General Electric F110 is an afterburning turbofan jet engine produced by GE Aerospace (formerly GE Aviation). It was derived from the General Electric F101 as an alternative engine to the Pratt & Whitney F100 for powering tactical fighter aircraft, with the F-16C Fighting Falcon and F-14A+/B Tomcat being the initial platforms; the F110 would eventually power new F-15 Eagle variants as well.
The first MSIP II F-16C Block 25 was delivered in July 1984. Block 30/32 takes advantage of the Alternative Fighter Engine program that offered a choice between two engines for the F-16: the General Electric F110-GE-100 (Block 30) as well as the newly upgraded Pratt & Whitney F100-PW-220 (Block 32).
General Electric and Pratt & Whitney are fighting over the next F-35 engine. It's the most expensive defense program in history, so the stakes are high.
The Air Force would award Pratt & Whitney a contract in 1970 to develop and produce F100-PW-100 (USAF) and F401-PW-400 (USN) engines. The Navy would use the engine in the planned F-14B and the XFV-12 project but would cut back and later cancel its order after the latter's failure due to costs and reliability issues, and chose to continue to use ...
The first F-16 AM was delivered in June 2003, and the FAP personnel performed the modification of the remaining 18 aircraft. Currently the Portuguese F-16 fleet uses the AN/ALQ-131 ECM pods, that had originally been bought for the A-7P Corsair IIs, and the new Rafael LITENING II targeting pods. One aircraft has been preserved for public display ...
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The F-16XL-2 also received a larger inlet which would go on to be included in later F-16 variants. [ 20 ] These changes resulted in a 25% improvement in lift-to-drag ratio in supersonic flight [ 21 ] while remaining comparable in subsonic flight, [ 22 ] and a plane that reportedly handled smoothly at high speeds and low altitudes. [ 23 ]