Aircraft Specification Sheet for the Grumman F-14 Tomcat
Prototype first flew :1970.
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Dimenstions
Version | First Flight in service | customers | Length | Height | Wing span (spread) | Wing span (swept) | Wing area |
Prototype | 1970 | ||||||
F-14A | 1970 | US NAVY,IRANIAN AF | 61 ft 11in (18,90m) | 16ft 0 in (4,88m) | 64 ft 1,5 in (19,55m) | 37 ft 7in (11,45m) | 565 sq ft (52,50mē) |
F-14B (PW engine) | 1973 | ||||||
F-14B | 1986 | US NAVY | 62 ft 8 in (19,10m) | 16ft 0 in (4,88m) | 64 ft 1.5 in (19,55m) | 38 ft 2.5 in (11,65m) | 565 sq ft (52,49mē) |
F-14D | 1990 | US NAVY | 62 ft 8 in (19,10m) | 16ft 0 in (4,88m) | 64 ft 1,5 in (19,55m) | 38 ft 2.5 in (11,65m) | 565 sq ft (52,49mē) |
Performance (Approx.)
Version | Engine | Thrust Dry | Thrust Reheat | endurance | ferry range | Crew | Max.Ceiling | Max.Speed |
Prototype | 2x Pratt & Whitney TF30-P412 turbofans | 20,900 lb (9.480 kg) | 450 mls (725 km) | 2 | 60,000 ft (18.290m) | 1,545 mph (2.486 km/h) | ||
F-14A | 2x Pratt & Whitney TF30-P412 turbofans | 20,900 lb (9.480 kg) | 450 mls (725 km) | 2 | 60,000 ft (18.290m) | 1,545 mph (2.486 km/h) | ||
F-14B (prototype) | 2x Pratt & Whitney F401-PW-400 turbofans | 28,096 lb (12.745 kg) | 2 | |||||
F-14B (production) | 2x General Electric F110-GE-400 turbofans | 14,000 lb (6.350 kg) | 23,100 lb (10.477 kg) | 510 mls (820 km) | 2 | 50,000 ft+ (15.200m) | 1,544 mph (2.485 km/h) | |
F-14D | 2x General Electric F110-GE-400 turbofans | 14,000 lb (6.350 kg) | 23,100 lb (10.477 kg) | 510 mls (820 km) | 2 | 50.000 ft+ (15.200m) | 1,544 mph (2.485 km/h) | |
Version | Armament | alternative Armament | ||||||
F-14A | 1x 20-mm M-61A1 rotary cannon | 6x AIM-7E/F Sparrow | 4x AIM-9G/H Sidewinder AAMs | 6x AIM-54A Phoenix | 2x AIM-9G/H Sidewinder AAMs | |||
F-14B | ||||||||
F-14D | 1 x 20-mm rotary cannon | 4x AIM-54C Phoenix | 4x AIM-7 Sparrow AAMs | 4x AIM9 Sidwwinder AAMs | ||||