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To meet Navy range and reserves requirements, McDonnell increased fuel capacity by 4,460 pounds (2,020 kg), by enlarging the dorsal spine and adding a 96-gallon fuel tank to each wing. A "snag" was added to the wing's leading edge and stabilators to prevent an aeroelastic flutter discovered in the F-15 stabilator. The wings and stabilators were ...
The F-18L combined the systems and twin-engine layout of the F-18 that Air Command favored with a lighter land-based equipment setup that significantly improved performance. Northrop, the primary contractor for the F-18L version, had not built the aircraft by the time of the NFA program, waiting on successful contracts before doing so.
The Hornet proved to be effective but limited in combat radius. The concept of an enlarged Hornet was first proposed in the 1980s, which was marketed by McDonnell Douglas as "Hornet 2000". The "Hornet 2000" concept was an advanced F/A-18 with a larger wing and a longer fuselage to carry more fuel and more powerful engines. [5] [6]
The General Electric F414 is an American afterburning turbofan engine in the 22,000-pound (98 kN) thrust class produced by GE Aerospace (formerly GE Aviation). The F414 originated from GE's widely used F404 turbofan, enlarged and improved for use in the Boeing F/A-18E/F Super Hornet.
The Super Hornet, developed in the 1990s as a jumbo version of the original F/A-18C Hornet, is the U.S. Navy’s main fighter jet. Barring an order from India, Boeing will pivot manpower and ...
Boeing F/A-18E/F Super Hornet; This page is a redirect. The following categories are used to track and monitor this redirect: From an alternative name: ...
An F/A-18E Super Hornet launching off the flight deck of a Nimitz-class aircraft carrier. U.S. Navy photo by Mass Communication Specialist 2nd Class Isaiah B. Goessl The air-to-air missile range ...
For the F/A-18, GE based the F404 on the YJ101 engine they had developed for the Northrop YF-17, enlarging the bypass ratio from 0.20 to 0.34 to enable higher fuel efficiency. The engine consists of a three-staged fan, seven axial stage compressor arrangement, single stage low and high pressure turbines, an augmentor, and produces maximum ...