Search filter

    • Year
      1906
      2018
    • Length
      23 m
      35 m
    • Height
      7 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      96 m2
      145 m2
    • Wingspan (Beam)
      24 m
      37 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
      18656 kg
      27984 kg
    • Max. takeoff weight (Gross weight)
      30960 kg
      46440 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      48 per.
      72 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      644 km/h
      968 km/h
    • Сruise Speed
      563 km/h
      845 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
      12160 l
      18240 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
      0 hp
      60000 hp
    • Thrust
      103 kN
      155 kN
    • Service ceiling
      9280 m
      13920 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1040 km
      1560 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
      854 m/min
      1282 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
      24 qt
      38 qt
    • Price
      34122240 USD
      51183360 USD

Kawasaki C-1

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
29
88.7
Height (m)
0.6
 
10.0
50.1
Wings
Wing area (m2)
1.1
 
120.5
925
Wingspan (Beam) (m)
0.1
 
30.6
95
Weights
Empty weight (kg)
8
 
23,320
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
38,700
575,000
Capacity
Crew (per.)
1
 
5
112
pilot, copilot, navigator, flight engineer, loadmaster
Capacity passengers (per.)
1
 
60
400
or 45 paratroopers, 36 patients with medics, or cargo
Speeds
Max. Speed (km/h)
25
 
806
28,165
at 7620 m at 35450 kg
Сruise Speed (km/h)
52
 
704
3,087
Fuel
Fuel Capacity (l)
23
 
15,200
320,000
Power
Thrust (kN)
1.5
 
129
1,914
2 powerplants 64,5 kN each
Performance
Service ceiling (m)
0.6
 
11,600
161,544
Range (Ferry range) (km)
4
 
1,300
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,068
36,000
Stat
Number built (qt)
0
 
31
43,000
Price (USD)
41.5
 
42.7 million
750.0 million
Introduction 1970
First flight 12.11.1970

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