Search filter

    • Year
      1906
      2018
    • Length
      14 m
      23 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      96 m2
      146 m2
    • Wingspan (Beam)
      21 m
      33 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
      3520 kg
      5280 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      6120 kg
      9180 kg
    • Crew
      3 per.
      5 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
      144 km/h
      216 km/h
    • Сruise Speed
      52 km/h
      3087 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
      960 hp
      1440 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4000 m
      6000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      528 km
      792 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
      1 m/min
      36000 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
      4 qt
      6 qt
    • Bombs
      1 qt
      2 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
      22 qt
      34 qt
    • Price
      41 USD
      750000000 USD

Kawasaki Ka 87

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
18.5
88.7
Height (m)
0.6
 
5.8
50.1
Wings
Wing area (m2)
1.1
 
121
925
Wingspan (Beam) (m)
0.1
 
26.8
95
Weights
Empty weight (kg)
8
 
4,400
276,800
Loaded weight (kg)
5
 
7,650
242,500
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
180
28,165
Power
Total Power (hp)
0.4
 
1,200
60,000
2 powerplants 600 hp each
Performance
Service ceiling (m)
0.6
 
5,000
161,544
Range (Ferry range) (km)
4
 
660
40,700
Combat
Guns (qt)
1
 
5
18
machine guns
Bombs (qt)
1
 
1
250
600 kg (1,320 lb) bomb
Stat
Number built (qt)
0
 
28
43,000
First flight 19.02.1926

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