Grumman F-14A "Tomcat" 
Grumman F-14A "Tomcat"
 
The F-14 has been the Navy’s primary air superiority fighter since it entered the fleet in the 1970’s.  Grumman won the VFX competition to develop this aircraft in 1969 and flew the first prototype F-14A in December 1970.

The F-14 was designed to fulfill the missions of clearing contested airspace and protecting strike forces, defending the carrier fleet, and secondary attack of tactical ground targets.

This two-seat carrier-based fighter utilizes variable-sweep wings to provide good aerodynamic performance at both low and high speeds.  A Mach Sweep Programmer selects the optimum sweep angle based on speed and altitude.  The aircraft has twin vertical tails with rudders and all-flying horizontal tails.  The large rectangular inlets utilize variable multiple shock ramps for good supersonic performance.

The F-14A at the Western Museum of Flight was accepted by the Navy on February 18, 1976.  A fire in the right hand engine on May 7, 1979 structurally weakened the aircraft, causing it to be relegated as a maintenance trainer for most of its service life.  The aircraft was last stationed at Naval Air Station Miramar.
 
 

F-14A "Tomcat" Specifications
Manufacturer
Grumman Aerospace Corporation, Bethpage, New York
Wing Span
64.1 feet unswept (20 deg) 
38.2 feet swept (68 deg)
Overall Length
62.0 feet
Overall Height
16.0 feet
Weight, Empty
40,104 pounds
Weight, Max T.O.
74,349  pounds
Speed (Maximum)
Mach 2.34 (max. design Mach Number)
Altutude (Maximum)
Above 56,000 feet
Powerplants
(2) Pratt & Whitney TF30-P-414A 
(20,900 # thrust with afterburning)
Armament
(1) GE M61-A1 Vulcan 20mm gun 
(4) Sparrow air-to-air missiles 
Phoenix air-to-air missiles 
One wing pylon per side for various stores 
(maximum external store weight of 14,500 pounds)
Number Built
Over 500 F-14A version
 
 
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Last Update on 2.11.99