Search filter

    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      3 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
      3 kg/m2
      829 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
      2020 kg
      3030 kg
    • Max. takeoff weight (Gross weight)
      2796 kg
      4194 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
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      464 km/h
      696 km/h
    • Сruise Speed
      320 km/h
      480 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
      1201 hp
      1802 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8800 m
      13200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1760 km
      2640 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1120 km
      1680 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
      668 m/min
      1002 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      4 min
      8 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
      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
      316 qt
      474 qt
    • Price
      41 USD
      750000000 USD

Kawasaki Ki-100

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.8
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
20
925
Wingspan (Beam) (m)
0.1
 
12
95
Weights
Empty weight (kg)
8
 
2,525
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,495
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
580
28,165
at 6000 m
Сruise Speed (km/h)
52
 
400
3,087
Power
Total Power (hp)
0.4
 
1,501.3
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
11,000
161,544
Range (Ferry range) (km)
4
 
2,200
40,700
Сombat radius (km)
277
 
1,400
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
835
36,000
Time to altitude (min)
0.6
 
6
105
to 5000 m
Combat
Guns (qt)
1
 
4
18
2 × 20 mm fuselage-mounted Ho-5 cannons, and 2 × 12.7 mm (.50 in) wing-mounted Ho-103 machine guns
Stat
Number built (qt)
0
 
395
43,000
Introduction 1945
First flight 01.02.1945
Stop production 1945

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