Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      27 m2
      42 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      344 kg/m2
      516 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
      7621 kg
      11433 kg
    • Max. takeoff weight (Gross weight)
      17680 kg
      26520 kg
    • Loaded weight
      11976 kg
      17964 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      1699 km/h
      2549 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
      4272 l
      6409 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      2 kN/kg
    • Afterburning thrust
      104 kN/kg
      158 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      60 kN
      91 kN
    • Service ceiling
      14400 m
      21600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      7 G
      9 G
    • Rate of climb
      1 m/min
      36000 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
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      6468 kg
      9702 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      75 qt
      113 qt
    • Price
      101600000 USD
      152400000 USD

Mitsubishi F-2

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
15.5
88.7
Height (m)
0.6
 
5.0
50.1
Wings
Wing area (m2)
1.1
 
34.8
925
Wingspan (Beam) (m)
0.1
 
11.1
95
Wing loading (kg/m2)
3.1
 
430
829
at weight of 15000 kg
Weights
Empty weight (kg)
8
 
9,527
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
22,100
575,000
Loaded weight (kg)
5
 
14,970
242,500
Capacity
Crew (per.)
1
 
1
112
2 for the F-2B
Speeds
Max. Speed (km/h)
25
 
2,124
28,165
Fuel
Fuel Capacity (l)
23
 
5,340.4
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.9
2.1
Afterburning thrust (kN/kg)
29.4
 
131.2
980
1 powerplant
Thrust (kN)
1.5
 
75.6
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
18,000
161,544
Dynamic Performance
Load factor from (G)
2
 
9
9
Combat
Guns (qt)
1
 
1
18
20 mm JM61A1 cannon
Bombs weight (kg)
2
 
8,085
39,000
of all weapon
Stat
Number built (qt)
0
 
94
43,000
Price (USD)
41.5
 
127.0 million
750.0 million
Introduction 1995
First flight 07.10.1995

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