Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      23 m2
    • Wingspan (Beam)
      9 m
      14 m
    • Wing loading
      59 kg/m2
      90 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      5
      9
    • 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
      856 kg
      1284 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1108 kg
      1662 kg
    • Crew
      1 per.
      3 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
      242 km/h
      364 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      180 km/h
      270 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      101 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
      1 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
      1 kN
      1914 kN
    • Service ceiling
      4880 m
      7320 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      912 km
      1368 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      134 m
      202 m
    • Landing roll
      164 m
      248 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      268 m/min
      404 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      1 m
      3 m
    • Prop blade number
      1 qt
      3 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Kawasaki KAT-1

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
8.5
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
18.6
925
Wingspan (Beam) (m)
0.1
 
11.5
95
Wing loading (kg/m2)
3.1
 
74.5
829
Aspect ratio
1.7
 
7.1
25.6
Weights
Empty weight (kg)
8
 
1,070
276,800
Loaded weight (kg)
5
 
1,385
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
303
1,500
Сruise Speed (km/h)
52
 
225
3,087
40% power at 2135 m
Landing Speed (km/h)
68
 
83.5
270
with flaps extended
Power
Power/mass (hp/kg)
0.0
 
0.2
22.1
Performance
Service ceiling (m)
0.6
 
6,100
161,544
Range (Ferry range) (km)
4
 
1,140
40,700
maximum at 40% power at 3050 m
Takeoff roll (m)
20
 
168
3,200
at sea level, no wind
Landing roll (m)
20
 
206
2,570
at sea level, no wind
Dynamic Performance
Rate of climb (m/min)
1.9
 
336
36,000
Propellers
Propellers (qt)
1
 
1
8
Prop diameter (m)
1.8
 
2.1
5.8
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
2
43,000
First flight 11.02.1954

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