Search filter

    • Year
      1906
      2018
    • Length
      10 m
      15 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      26 m2
      41 m2
    • Wingspan (Beam)
      12 m
      19 m
    • Wing loading
      210 kg/m2
      316 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
      4784 kg
      7176 kg
    • Max. takeoff weight (Gross weight)
      7544 kg
      11316 kg
    • Loaded weight
      7036 kg
      10554 kg
    • Crew
      1 per.
      3 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
      564 km/h
      846 km/h
    • Сruise Speed
      360 km/h
      540 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
      29 kN/kg
      980 kN/kg
    • Total Power
      3312 hp
      4968 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      10080 m
      15120 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1562 km
      2344 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
      1018 m/min
      1528 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      8 min
      12 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      3 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
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi Ki-83

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
12.5
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
33.5
925
Wingspan (Beam) (m)
0.1
 
15.5
95
Wing loading (kg/m2)
3.1
 
263
829
Weights
Empty weight (kg)
8
 
5,980
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
9,430
575,000
Loaded weight (kg)
5
 
8,795
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
705
28,165
at 9000 m
Сruise Speed (km/h)
52
 
450
3,087
Power
Total Power (hp)
0.4
 
4,140
60,000
2 powerplants 2070 hp each at 1000 m
Performance
Service ceiling (m)
0.6
 
12,600
161,544
Range (Ferry range) (km)
4
 
1,953
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,273
36,000
Time to altitude (min)
0.6
 
10
105
to 10000 m
Combat
Guns (qt)
1
 
2
18
30 mm (1.18 in) and 2× 20 mm cannon mounted in the fuselage nose
Stat
Number built (qt)
0
 
4
43,000
Introduction 1944
First flight 18.11.1944

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