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    • Year
      1906
      2018
    • Length
      16 m
      26 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      48 m2
      74 m2
    • Wingspan (Beam)
      17 m
      26 m
    • Wing loading
      562 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      16728 kg
      25092 kg
    • Max. takeoff weight (Gross weight)
      31932 kg
      47900 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      4 qt
      8 qt
    • Ground Speed
      1004 km/h
      1500 km/h
    • Max. Speed
      1864 km/h
      2796 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      23 l
      320000 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      1 kN/kg
    • Afterburning thrust
      131 kN/kg
      198 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      76 kN
      115 kN
    • Service ceiling
      15849 m
      23775 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2712 km
      4068 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      5193 m/min
      7791 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      4 qt
      8 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      5 qt
      9 qt
    • Price
      6400000 USD
      9600000 USD

General Dynamics F-111

TypeAircraft
Company

General Dynamics

Grumman Aerospace Corporation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
21.0
88.7
Height (m)
0.6
 
4.8
50.1
Wings
Wing area (m2)
1.1
 
51.1
925
Swept
1.1
 
60.9
925
Spread
Wingspan (Beam) (m)
0.1
 
10.3
95
Swept
0.1
 
21.3
95
Spread
Wing loading (kg/m2)
3.1
 
586
829
Spread
3.1
 
703
829
Swept
Weights
Empty weight (kg)
8
 
20,910
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
39,916.1
575,000
Capacity
Crew (per.)
1
 
2
112
pilot and weapons system operator
Hardpoints (qt)
1
 
6
2,576
Speeds
Ground Speed (km/h)
96.6
 
1,255
1,500
Max. Speed (km/h)
25
 
2,330
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.5
2.1
Afterburning thrust (kN/kg)
29.4
 
164.6
980
2 powerplants 82,3 kN each
Thrust (kN)
1.5
 
95.6
1,914
2 powerplants 47,8 kN each
Performance
Service ceiling (m)
0.6
 
19,812
161,544
Range (Ferry range) (km)
4
 
3,390
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
6,492.2
36,000
Combat
Guns (qt)
1
 
1
18
M61 Vulcan 20 mm (0.787 in) Gatling cannon (seldom fitted)
Missiles (qt)
1
 
6
24
AIM-54 Phoenix long range air-air missiles (four under wings, two in weapons bay)
Stat
Number built (qt)
0
 
7
43,000
Price (USD)
41.5
 
8.0 million
750.0 million
Introduction 1965
First flight 18.05.1965

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