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The Super Hornet is an enlarged redesign of the McDonnell Douglas F/A-18 Hornet.The wing and tail configuration trace its origin to a Northrop prototype aircraft, the P-530, c. 1965, which began as a rework of the lightweight Northrop F-5E (with a larger wing, twin tail fins and a distinctive leading edge root extension, or LERX). [4]
The Super Hornet, which began production in 1995, has a new, 25% larger airframe, larger rectangular air intakes, more powerful GE F414 engines based on F/A-18's F404, and an upgraded avionics suite. Like the Marine Corps' F/A-18D, the Navy's F/A-18F carries a naval flight officer as a second crew member in a weapon systems officer (WSO) role.
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.
A United States Marine Corps F/A-18 fighter-attack jet crashes, killing a student pilot and injuring a flight instructor. The aircraft had taken off from the Marine Corps Air Station in Yuma but was from Marine Fighter Attack Training Squadron 101, stationed in San Diego. Capt. Douglas F. Aguilera, 33, of Paso Robles, Calif., was killed. Maj.
An intake ramp is a rectangular, plate-like device within the air intake of a jet engine, designed to generate a number of shock waves to aid the inlet compression process at supersonic speeds. [1] The ramp sits at an acute angle to deflect the intake air from the longitudinal direction. [ 2 ]
The McDonnell Douglas CF-18 Hornet (official military designation CF-188) is a Royal Canadian Air Force (RCAF) variant of the American McDonnell Douglas F/A-18 Hornet fighter aircraft. In 1980, the F/A-18 was selected as the winner of the New Fighter Aircraft Project competition to replace CF-104 Starfighter, CF-101 Voodoo and the CF-116 ...
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The air intake (inlet U.S. [6]) is an aerodynamic duct extending from an entry lip to the engine fan/compressor. For supersonic intakes with variable geometry it is called an intake system, referring to the need for shock-wave and internal duct flow management using variable position surfaces (ramps or cones) and bypass doors. [7]
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