Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 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
      80 m2
      121 m2
    • Main rotor diameter
      9 m
      14 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
      652 kg
      980 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1034 kg
      1552 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      2 per.
      4 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      135 km/h
      203 km/h
    • Сruise Speed
      112 km/h
      168 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
      216 hp
      324 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4512 m
      6768 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      320 km
      480 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      3 h
      5 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
      206 m/min
      310 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 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
      168 qt
      254 qt
    • Price
      41 USD
      750000000 USD

Kawasaki KH-4

TypeHelicopter
Company

Kawasaki Heavy Industries

Geometry
Length (m)
1.9
 
9.9
88.7
Height (m)
0.6
 
2.8
50.1
Rotors
Disc area (m2)
1.4
 
100.6
460
Main rotor diameter (m)
1.2
 
11.3
62
Weights
Empty weight (kg)
8
 
816
276,800
Loaded weight (kg)
5
 
1,293
242,500
Capacity
Capacity passengers (per.)
1
 
3
400
Speeds
Max. Speed (km/h)
25
 
169
28,165
Сruise Speed (km/h)
52
 
140
3,087
Power
Total Power (hp)
0.4
 
270
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,640
161,544
Range (Ferry range) (km)
4
 
400
40,700
Endurance (h)
0.0
 
4.1
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
258
36,000
Stat
Number built (qt)
0
 
211
43,000
First flight 01.08.1962

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