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RADMRockstone — Grumman F-14A ''Tomcat'' (VF-84)

Published: 2020-09-20 15:20:55 +0000 UTC; Views: 14865; Favourites: 188; Downloads: 0
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Description The Grumman F-14A ''Tomcat'' is an American supersonic, twin-engine, two-seat, twin-tail, variable-sweep wing fighter aircraft. The Tomcat was developed for the United States Navy's Naval Fighter Experimental (VFX) program after the collapse of the F-111B project. The F-14A was the first of the American Teen Series fighters, which were designed incorporating air combat experience against MiG fighters during the Vietnam War. 

The F-14 first flew on 21 December 1970 and made its first deployment in 1974 with the U.S. NAVY aboard USS ''Enterprise'' (CVN-65), replacing the McDonnell Douglas F-4 ''Phantom II''. The F-14A served as the U.S. NAVY's primary maritime air superiority fighter, fleet defense interceptor, and tactical aerial reconnaissance platform into the 2000s. The Low Altitude Navigation and Targeting Infrared for Night (LANTIRN) pod system was added in the 1990s and the ''Tomcat'' began performing precision ground-attack missions. 


In the 1980s, F-14As were used as land-based interceptors by the Islamic Republic of Iran Air Force during the Iran-Iraq War, where they saw combat against Iraqi warplanes. Iranian F-14s reportedly shot down at least 160 Iraqi aircraft during the war, while only 12 to 16 ''Tomcats'' were lost; at least half of these losses were due to accidents.


The F-14A ''Tomcat'' was designed as both an air superiority fighter and a long-range naval interceptor, which enabled it to both serve as escort attack aircraft when armed with Sparrow missiles and fleet air defense loitering interceptor role when armed with Phoenix missiles. The F-14A was designed with a two-seat cockpit with a bubble canopy which affords all-around visibility aiding aircrew in air-to-air combat. It features variable geometry wings that swing automatically during flight. For high-speed intercept, they are swept back and they swing forward for lower speed flight. It was designed to improve on the F-4 ''Phantom's'' air combat performance in most respects.

The F-14's fuselage and wings allow it to climb faster than the F-4, while the twin-tail arrangement offers better stability. The F-14A is equipped with an internal 20 mm M61 Vulcan Gatling cannon mounted on the left side (unlike the Phantom, which was not equipped with an internal gun in the U.S.NAVY), and can carry AIM-54 ''Phoenix'', AIM-7 ''Sparrow'', and AIM-9 ''Sidewinde''r anti-aircraft missiles. The twin engines are housed in widely spaced nacelles. The flat area of the fuselage between the nacelles is used to contain fuel and avionics systems, such as the wing-sweep mechanism and flight controls, as well as weaponry since the wings are not used for carrying ordnance. By itself, the fuselage provides approximately 40 to 60 percent of the F-14A's aerodynamic lifting surface depending on the wing sweep position. The lifting body characteristics of the fuselage allowed one F-14A to safely land after suffering a mid-air collision that sheared off more than half of the plane's right wing in 1991.


The F-14A began replacing the F-4 ''Phantom II'' in U.S. NAVY service starting in September 1974 with squadrons VF-1 "Wolfpack" and VF-2 "Bounty Hunters" aboard USS Enterprise and participated in the American withdrawal from Saigon. The F-14A had its first kills in U.S. Navy service on 19 August 1981 over the Gulf of Sidra in what is known as the Gulf of Sidra incident. In that engagement, two F-14As from VF-41 ''Black Aces'' were engaged by two Libyan Su-22 "Fitters". The F-14As evaded the short range heat seeking AA-2 "Atoll" missile and returned fire, downing both Libyan aircraft. U.S. Navy F-14s once again were pitted against Libyan aircraft on 4 January 1989, when two F-14s from VF-32 shot down two Libyan MiG-23 "Floggers" over the Gulf of Sidra in a second Gulf of Sidra incident.

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tigermki [2021-05-23 22:20:40 +0000 UTC]

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