Search filter

    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      24 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      138 kg/m2
      209 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
      2104 kg
      3156 kg
    • Max. takeoff weight (Gross weight)
      3060 kg
      4590 kg
    • Loaded weight
      2776 kg
      4164 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
      464 km/h
      696 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
      928 hp
      1392 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9280 m
      13920 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      464 km
      696 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      880 km
      1320 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
      729 m/min
      1095 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      9 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      3 qt
      5 qt
    • Bombs
      1 qt
      3 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
      2527 qt
      3791 qt
    • Price
      41 USD
      750000000 USD

Kawasaki Ki-61

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.9
88.7
Height (m)
0.6
 
3.7
50.1
Wings
Wing area (m2)
1.1
 
20
925
Wingspan (Beam) (m)
0.1
 
12
95
Wing loading (kg/m2)
3.1
 
173.5
829
Weights
Empty weight (kg)
8
 
2,630
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,825
575,000
Loaded weight (kg)
5
 
3,470
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
580
28,165
at 5000 m
Сruise Speed (km/h)
52
 
450
3,087
Power
Total Power (hp)
0.4
 
1,158.2
60,000
0.4
 
1,160
60,000
1 powerplants
Performance
Service ceiling (m)
0.6
 
11,600
161,544
Range (Ferry range) (km)
4
 
580
40,700
Сombat radius (km)
277
 
1,100
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
912
36,000
Time to altitude (min)
0.6
 
7
105
to 5000 m
Combat
Guns (qt)
1
 
4
18
2× 20 mm Ho-5 cannon, 120 rpg each; 2× 12.7 mm (0.50 in) Ho-103 machine guns, 250 rpg each
Bombs (qt)
1
 
2
250
250 kg (551 lb) bombs
Stat
Number built (qt)
0
 
3,159
43,000
Introduction 1941
First flight 01.12.1941
Stop production 1945

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