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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      3 m
      5 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
      1 m2
      460 m2
    • Main rotor diameter
      8 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
      1 m
      3 m
    • Empty weight
      1381 kg
      2073 kg
    • Max. takeoff weight (Gross weight)
      2680 kg
      4020 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
      25 km/h
      28165 km/h
    • Сruise Speed
      198 km/h
      298 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
      222 km/h
      334 km/h
    • Fuel Capacity
      557 l
      837 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
      948 hp
      1424 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3660 m
      5490 m
    • Static ceiling
      2052 m
      3078 m
    • Range (Ferry range)
      432 km
      650 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
      528 m/min
      792 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Kawasaki BK 117

TypeHelicopter
Company

Kawasaki Heavy Industries

Messerschmitt-Bölkow-Blohm

Geometry
Length (m)
1.9
 
9.9
88.7
fuselage length
Height (m)
0.6
 
3.9
50.1
rotors turning
Rotors
Main rotor diameter (m)
1.2
 
11
62
Tail rotor diameter (m)
0.8
 
2.0
4.9
Weights
Empty weight (kg)
8
 
1,727
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,350
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Сruise Speed (km/h)
52
 
250
3,087
52
 
248
3,087
Never exceed speed (km/h)
108.0
 
278
1,050
Fuel
Fuel Capacity (l)
23
 
697
320,000
internal fuel
Power
Total Power (hp)
0.4
 
1,186
60,000
2 powerplants 593 hp each
Performance
Service ceiling (m)
0.6
 
4,575
161,544
max certified altitud
Static ceiling (m)
3
 
2,565
5,485
in ground effect
Range (Ferry range) (km)
4
 
541
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
660
36,000
Stat
Introduction 13.06.1979

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