Grumman F-14 Tomcat
Twin-Turbofan Long-Range Interceptor and Tactical Reconnaissance Aircraft
Technical Data
Powerplants: Two General Electric F100-GE-400 afterburning turbofans
Developing: 102.75kN (23,000lb st) with afterburner
Span: 19.54m (64ft 1.5in) wings spread
Length: 19.10m (62ft 8in)
Height: 4.88m (16ft 0in)
All-up weight: 33,724kg (74,349lb)
Maximum speed: 1,997km/h (1,241mph)
Cruise speed: 764km/h (475mph)
Operational ceiling: Over 53,000ft
Maximum range: 2,965km (1,840miles)
Accommodation: Pilot and radar intercept officer in tandem
Warload: Two AIM-9M Sidewinders are carried for close-range combat purposes, while up to six (but more usually two-four) AIM-54C Phoenix or AIM-7M Sparrow AAMs are used for long-range engagements. An M61A1 Vulcan 20mm six-barrelled cannon is mounted to port in the lower forward fuselage. The F-14 can also be fitted with bomb rack in its semi-recessed missile bays, which normally carry four of the Phoenix or Sparrow missiles, to deliver various free-fall general purpose stores.
First flown: 21 December 1970 (F-14 prototype); September 1986 (F-14A (plus))
Entered service: October 1972 (F-14A); 1988 (F-14B)
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