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Since the LWF did not share the design requirements of the VFAX, the Navy asked McDonnell Douglas and Northrop to develop a new aircraft from the design and principles of the YF-17. On 1 March 1977, Secretary of the Navy W. Graham Claytor announced, that the F-18 would be named "Hornet", after the characteristics of the Hornet insect.
Candidates included the Grumman F-14 Tomcat, McDonnell Douglas F-15 Eagle, Panavia Tornado, Dassault Mirage F1 (later replaced by the Mirage 2000), plus the products of the American Lightweight Fighter (LWF) competition, the General Dynamics F-16 Fighting Falcon, the F/A-18 Hornet, and a de-navalized version of the Hornet, the Northrop F-18L ...
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.
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 ...
With a fuel fraction of nearly 85%, the GlobalFlyer could carry 5 times its weight in fuel.. In aerospace engineering, an aircraft's fuel fraction, fuel weight fraction, [1] or a spacecraft's propellant fraction, is the weight of the fuel or propellant divided by the gross take-off weight of the craft (including propellant): [2]
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 ...
1.07 With full fuel Dassault Rafale: 0.988 [10] Version M, 100% fuel, 2 EM A2A missile, 2 IR A2A missiles Sukhoi Su-30MKM: 1.00 [11] Loaded weight with 56% internal fuel McDonnell Douglas F-15: 1.04 [12] Nominally loaded Mikoyan MiG-29: 1.09 [13] Full internal fuel, 4 AAMs Lockheed Martin F-22 >1.09 (1.26 with loaded weight and 50% fuel) [14 ...