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    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      40 m2
      62 m2
    • Wingspan (Beam)
      15 m
      24 m
    • Wing loading
      125 kg/m2
      189 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
      3737 kg
      5607 kg
    • Max. takeoff weight (Gross weight)
      6420 kg
      9630 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      1920 kg
      2880 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      11 per.
      17 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      320 km/h
      480 km/h
    • Сruise Speed
      293 km/h
      441 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
      1584 hp
      2376 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6400 m
      9600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2640 km
      3960 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
      192 m/min
      288 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      10 min
      16 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      18 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
      96 qt
      146 qt
    • Price
      41 USD
      750000000 USD

Kawasaki Ki-56

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
14.9
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
51.2
925
Wingspan (Beam) (m)
0.1
 
20.0
95
Wing loading (kg/m2)
3.1
 
156.7
829
Weights
Empty weight (kg)
8
 
4,672
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,025
575,000
Capacity
Crew (per.)
1
 
3
112
pilot, co-pilot, navigator, & radio operator
Useful load (kg)
26.4
 
2,400
90,700
Capacity passengers (per.)
1
 
14
400
Speeds
Max. Speed (km/h)
25
 
400
28,165
at 3500 m
Сruise Speed (km/h)
52
 
367
3,087
Power
Total Power (hp)
0.4
 
1,980
60,000
2 powerplants 990 hp each
Performance
Service ceiling (m)
0.6
 
8,000
161,544
Range (Ferry range) (km)
4
 
3,300
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
240
36,000
Time to altitude (min)
0.6
 
12.6
105
to 3000 m
Stat
Number built (qt)
0
 
121
43,000
Introduction 1940

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