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McDonnell Douglas F/A-18 Hornet

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McDonnell Douglas F/A-18 Hornet
NameF/A-18 Hornet
CaptionA United States Navy F/A-18C in flight.
TypeMultirole fighter
National originUnited States
ManufacturerMcDonnell Douglas / Northrop, Boeing / Northrop Grumman
First flight18 November 1978
Introduction7 January 1983
Retired2023 (United States Marine Corps)
StatusIn service with other operators
Primary userUnited States Navy (historical)
More usersRoyal Australian Air Force, Spanish Air and Space Force, Finnish Air Force
Number builtc. 1,480
Developed fromNorthrop YF-17
Developed intoBoeing F/A-18E/F Super Hornet, Boeing EA-18G Growler

McDonnell Douglas F/A-18 Hornet is a twin-engine, supersonic, all-weather, carrier-capable, multirole combat jet. Designed as both a fighter and attack aircraft, it was developed for the United States Navy and United States Marine Corps from the Northrop YF-17. The Hornet entered service in the 1980s and became a cornerstone of U.S. Navy and U.S. Marine Corps aviation, seeing extensive combat and serving with numerous allied nations.

Development and origins

The Hornet's genesis lies in the Lightweight Fighter program of the early 1970s, which produced the General Dynamics YF-16 and the Northrop YF-17. While the United States Air Force selected the YF-16, the United States Navy sought a new multirole aircraft for its Naval Air Systems Command. McDonnell Douglas partnered with Northrop Corporation to adapt the YF-17 design for carrier operations, leading to the F/A-18. Key changes included a strengthened airframe, arresting hook, and landing gear for carrier landings. The program was managed by the U.S. Department of Defense and faced significant cost overruns and development challenges, as documented in reports to the United States Congress.

Design and variants

The Hornet features a semi-monocoque fuselage, leading-edge extensions, and twin vertical stabilizers canted outward. Its design emphasizes excellent slow-speed handling and angle of attack performance, crucial for carrier operations. The initial single-seat F/A-18A and twin-seat F/A-18B were followed by the improved F/A-18C and F/A-18D models, which incorporated upgraded avionics, Hughes AN/APG-73 radar, and expanded weapons capability for AIM-120 AMRAAM and AGM-65 Maverick missiles. A dedicated reconnaissance version, the RF-18, was used by the Finnish Air Force. The most significant evolution was the larger, more capable Boeing F/A-18E/F Super Hornet, developed by Boeing after its merger with McDonnell Douglas.

Operational history

The Hornet first saw combat in 1986 during Operation Prairie Fire and Operation El Dorado Canyon against Libya. It served extensively during the Gulf War, conducting both air superiority and strike fighter missions over Iraq and Kuwait. United States Navy and United States Marine Corps Hornets were pivotal in enforcing the no-fly zone over Bosnia and Herzegovina and during Operation Allied Force in Kosovo. The aircraft saw continuous use in the War in Afghanistan and the Iraq War, providing close air support. Notable combat losses included one to a MiG-25 during the Gulf War and another in the 1999 NATO bombing of Yugoslavia.

Operators

The primary operator was the United States Navy, which flew the Hornet from carriers like the USS Nimitz and USS Theodore Roosevelt. The United States Marine Corps operated both single and two-seat models until its retirement of the type in 2023. Major international operators have included the Royal Australian Air Force, which flew them from HMAS Melbourne and later the Canberra-class landing helicopter dock, and the Spanish Air and Space Force, which designated them as the EF-18 and operated from Base Aérea de Torrejón. Other operators include the Finnish Air Force, the Swiss Air Force, the Royal Canadian Air Force, and the Kuwait Air Force.

Specifications (F/A-18C/D)

* **Crew:** 1 (C model), 2 (D model) * **Length:** 56 ft 0 in (17.07 m) * **Wingspan:** 40 ft 5 in (12.31 m) with AIM-7 Sparrow missiles * **Height:** 15 ft 4 in (4.66 m) * **Empty weight:** 24,700 lb (11,200 kg) * **Max takeoff weight:** 51,900 lb (23,541 kg) * **Powerplant:** 2 × General Electric F404-GE-402 turbofan engines * **Maximum speed:** Mach 1.8 (1,190 mph, 1,915 km/h) at 40,000 ft (12,190 m) * **Combat range:** 400 nmi (460 mi, 740 km) on a hi-lo-hi mission * **Service ceiling:** 50,000 ft (15,000 m) * **Armament:** 1 × 20 mm (0.787 in) M61 Vulcan rotary cannon, 9 hardpoints for up to 13,700 lb (6,215 kg) of ordnance including AIM-9 Sidewinder, AIM-120 AMRAAM, AGM-84 Harpoon, and AGM-88 HARM missiles. * **Avionics:** AN/APG-73 radar, AN/ALR-67 radar warning receiver, AN/ASQ-173 Laser Target Designator.

Category:Carrier-based aircraft Category:Multirole combat aircraft Category:McDonnell Douglas aircraft