Search filter

    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      26 m2
    • Wingspan (Beam)
      6 m
      10 m
    • Wing loading
      516 kg/m2
      774 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
      5086 kg
      7630 kg
    • Max. takeoff weight (Gross weight)
      10939 kg
      16409 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      5 qt
      9 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      1360 km/h
      2040 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
      3 kN/kg
    • Afterburning thrust
      56 kN/kg
      86 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      36 kN
      55 kN
    • Service ceiling
      12192 m
      18288 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2296 km
      3444 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      444 km
      668 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
      5664 m/min
      8496 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      1 min
      3 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      61 qt
      93 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi F-1

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
17.9
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
21.2
925
Wingspan (Beam) (m)
0.1
 
7.9
95
Wing loading (kg/m2)
3.1
 
645
829
Weights
Empty weight (kg)
8
 
6,358
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
13,674
575,000
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
7
2,576
One, centerline, four underwing and two wingtip missile rails
Speeds
Max. Speed (km/h)
25
 
1,700
28,165
at 11000 m
Power
Afterburning thrust (kN/kg)
29.4
 
71.2
980
2 powerplants 35,6 each
Thrust (kN)
1.5
 
45.6
1,914
2 powerplants 22,8 each
Performance
Service ceiling (m)
0.6
 
15,240
161,544
Range (Ferry range) (km)
4
 
2,870
40,700
with max external fuel
Сombat radius (km)
277
 
556
7,210
High-Low-High profile with two ASM-1 missiles and one 830 L drop tank
Dynamic Performance
Rate of climb (m/min)
1.9
 
7,080
36,000
Time to altitude (min)
0.6
 
2
105
to 11000 m
Combat
Guns (qt)
1
 
1
18
20 mm (0.787 in) JM61A1 Vulcan 6-barreled Gatling cannon
Stat
Number built (qt)
0
 
77
43,000
Introduction 1975
First flight 03.06.1975
Stop production 01.03.2006

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