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The modified F-16 demonstrated a maximum speed of Mach 2.0 (Mach 2.0 is the F-16's clean certified maximum speed) and handling characteristics similar to a normal F-16. Subsonic specific excess power was slightly improved. The trade studies involved additional CFD, testing, and weight and cost analyses.
The General Dynamics F-16XL is a derivative of the F-16 Fighting Falcon with a cranked-arrow delta wing. It entered the United States Air Force's (USAF) Enhanced Tactical Fighter (ETF) competition in 1981 but lost to the F-15E Strike Eagle. The two prototypes were shelved until being turned over to NASA for additional aeronautical research in 1988.
It was installed on an F-16 Block 30 fighter, replacing the aircraft's original intake diverter. The modified F-16 demonstrated a maximum speed of Mach 2.0 (Mach 2.0 is the F-16's clean certified maximum speed) and handling characteristics similar to a normal F-16. It was also shown that subsonic specific excess power was slightly improved.
The Mitsubishi F-2 is a multirole fighter derived from the General Dynamics F-16 Fighting Falcon, and manufactured by Mitsubishi Heavy Industries and Lockheed Martin for the Japan Air Self-Defense Force, with a 60/40 split in manufacturing between Japan and the United States.
A former United States Navy A4 Skyhawk on loan to the RNZAF Museum. It is displayed in the early RNZAF Colour Scheme at the Air Force Museum of New Zealand. In May 2001 the Fifth Labour Government of New Zealand decided to disband the Royal New Zealand Air Force's air combat force by withdrawing its Douglas A-4K Skyhawk fighter aircraft and Aermacchi MB-339 trainers without replacement. [1]
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The MiG-35 was a contender with the Eurofighter Typhoon, Boeing F/A-18E/F Super Hornet, Dassault Rafale, Saab JAS 39 Gripen, and General Dynamics F-16 Fighting Falcon in the Indian MRCA competition for 126 multirole combat aircraft to be procured by the Indian Air Force. Deficiencies with the MiG-35's radar and its RD-33MK engines led to the ...
It is the second of the BrahMos series of cruise missiles. The BrahMos-II is expected to have a range of 1,000 km (620 mi; 540 nmi) and a speed of Mach 8. During the cruise stage of flight, the missile will be propelled by a scramjet airbreathing jet engine. Other details, including production cost and physical dimensions of the missile, are ...