Grumman F-14A Tomcat
Carrier-based multi-role strike fighter
Crew: Two: pilot and radar intercept officers

Dimensions:
Wingspan (unswept): 64 ft., 1.5 in.
Wingspan (swept): 38 ft., 2.5 in.
Wingspan (overswept): 33 ft., 3.5 in.
Wing aspect ratio: 7.28
Length: 62 ft., 8 in.
Height: 16 ft.
Reference wing area: 565 sq ft.

Propulsion:
2 Pratt & Whitney TF30-P-414A
Military thrust per engine:
10,875 lbs.
Afterburner thrust per engine:
17,077 lbs.

Speeds:
No Tanks:
50,000 feet = Mach 1.87
25,000 feet = Mach 1.7
10,000 feet = Mach 1.35
With Tanks:
50,000 feet = Mach 1.7
25,000 feet = Mach 1.45
10,000 feet = Mach 1.1

Manuvering Speeds:
440-480kts FL200-FL500
440kts FL200 and below

Approach Speeds:
Landing Gear extention = 280 KIAS
Flaps and slats = 225 KIAS

Landing Speeds:
VR ref:130-142 KIAS @ 54,000 pounds,
VR ref:140-150 @ 60,000 lbs
Field takeoff distance: 2500 ft.
Field landing distance: 2400 ft.

Weights: Air Defense/Max Fuel
BOW 30,000 lbs.
Default Payoad 11,763 lbs.
MAX Payload 14,500 lbs.
MAX ZFW 42,000 lbs.

4 Internal Tanks 16,104 lbs. 2440 gal.
2 External Tanks 3,696 lbs. 560 gal.
Max Fuel 19,800 lbs. 3000 gal.

MTOW 74,349 lbs.
Carrier Landing 54,000 lbs.
Field Landing 60,000 lbs.
EMG Landing 72,000 lbs.

Range:
Maximum range:
1600 nm with full payload
2000 nm with full tanks
Service ceiling: 53,000 ft.
Econ: Angels 20 at 335kts.- mach.72


Armament: See the aircraft.cfg file

Internal:

M61A1 Vulcan 20 mm Gatling Gun
Feed System: 270 lbs
Gun: 252 lbs
Ammunition: 319 lbs
Total: 841 lbs

External:

External Camera/Fuel Tanks
Weight 218 lbs each

Air-to-air missiles:

AIM-7 Sparrow
Primary Function: Air-to-air guided missile
Contractor: Raytheon Co.
Power Plant: Hercules MK-58 solid-propellant rocket motor
Thrust: Classified
Speed: Classified
Range: Classified
Length: 12 ft
Diameter: 8 inches
Wingspan: 3 ft, 4 inches
Warhead: Annular blast fragmentation warhead
Launch Weight: 500 lbs
Guidance System: Raytheon semiactive on either continuous wave or pulsed Doppler radar energy
Date Deployed: AIM-7F, 1976; AIM-7M, 1982
Unit Cost: Approximately $125,000
Inventory: Classified

AIM-9 Sidewinders
Primary Function: Air-to-air missile
Contractor: Raytheon Co.; Ford Aerospace and Communications Corp.; Loral
Power Plant: Thiokol Hercules and Bermite MK 36 Mod 11; single-stage, solid-propellant rocket motor
Length: 9 ft 6 inches
Diameter: 5 inches
Fin Span: 2 ft 1 inch
Speed: Supersonic
Warhead: Blast fragmentation (conventional) weighing 20.8 pounds (9.36 kg)
Launch Weight: 190
Range: 8.7 nm
Guidance System: Solid-state infrared homing system
Unit Cost: $41,300
Date Deployed: 1956

6 AIM- 20 AMRAM
Primary Function: Medium-range, air-to-air tactical missile
Contractor: Hughes/Raytheon
Power Plant: High performance, directed rocket motor
Length: 12 feet
Launch Weight: 335 lbs
Diameter: Seven inches
Wing Span: 21 inches
Speed: Supersonic
Warhead: Blast Fragmentation; high explosive
Unit Cost: $386,000
Date Deployed: September 1991

AIM-54 Phoenix
Primary Function: Long-range air-launched air intercept missile
Contractor: Hughes Aircraft Co. and Raytheon Co.
Unit Cost: $477,131
Power Plant: Solid propellant rocket motor built by Hercules
Length: 13 ft
Weight: 1,024 lbs
Diameter: 15 inches
Wing Span: 3 ft
Range: In excess of 100 nm
Speed: In excess of 4,800 kmph
Guidance System: Semi-active and active radar homing
Warheads: Proximity fuse, high explosive
Warhead Weight: 135 lbs
Date Deployed: 1974

Air-to-ground weapons:

AGM-65E Maverick
Seeker: TV with
magnification
Speed: Mach 0.65
Length: 8 ft 2 in
Weight: 464 lbs
Warhead: 125 lbs
shaped charge
Range: 0.6 to 14 nm
Diameter:
Drag factor: 46

AGM-84D Harpoon
Primary Function: Anti-ship cruise missile.
Contractor: The Boeing Company
Power Plant: Teledyne Turbojet
Thrust: 660 lbs
Length: 12 ft, 7 inches
Weight: 1,145 lbs
Diameter: 13.5 inches
Wing Span: 3 ft
Range: Over-the-horizon, in excess of 60 nautical miles.
Speed: High Subsonic
Guidance: Sea-skimming cruise monitored by radar altimeter, active radar terminal homing.
Warhead: Penetration high-explosive blast at 488 lbs
Unit Cost: $720,000
Date Deployed: 1985


HGM-88 HARM
Primary Function: Air-to-surface anti-radiation missile.
Contractor: Raytheon
Power Plant: Thiokol dual-thrust, solid propellent, rocket motor
Length: 13 ft, 8 inches
Launch Weight: 800 lbs
Diameter: 10 inches
Wing Span: 3 ft, 8 inches
Range: 57+ nm
Speed: 1,216 kmph
Guidance: radar homing
Warhead: Blast fragmentation; warhead weight 150 lbs
Unit Cost: $284,000
Date Deployed: 1985

Mk82
Type: 500 lb class general-purpose iron bomb
Length: 7 ft 2 in
Weight: 531 lbs
Warhead: 275 lbs H-6 high-explosive
Drag factor: 40

Mk82HD Snakeye
Type: 500 lb class high-drag iron bomb
Length: 7 ft 6 in
Weight: 570 lbs
Warhead: 275 lbs H-6 high-explosive
Drag factor: 40

Mk83
Type: 1,000 lb class general-purpose iron bomb
Length: 9 ft 11 in
Weight: 985 lbs
Warhead: 416 lbs H-6 high-explosive
Drag factor: 50

Mk84
Type: 2,000 lb class general-purpose iron bomb
Length: 12 ft 9 in
Weight: 1,972 lbs
Warhead: 945 lbs H-6 high-explosive
Drag factor: 60

GBU-15 Guided Bomb Unit
Type: TV guided bomb
Length: 12 ft 10 in
Weight: 2,510 lbs
Warhead: 945 lbs H-6 high-explosive
Range: 5 miles
Drag factor: 46

CBU-84 Cluster Bomb Unit
Type: Sub-munitions dispenser
Length: 7 ft 8 in
Weight: 960 lbs
Warhead: 202 combined-effect bomblets
Drag factor: 50

BLU-107/B Durandal
Type: Anti-runway cratering bomb
Length: 8 ft 2 in
Weight: 450 lbs
Warhead: 330 lbs high-explosive
Drag factor: 40