Search filter

    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      15 m2
      24 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      65 kg/m2
      98 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
      2 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
      888 kg
      1332 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      12800 kg
      19200 kg
    • Crew
      1 per.
      112 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
      234 km/h
      352 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      168 km/h
      252 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
      240 l
      360 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
      192 hp
      288 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3600 m
      5400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      225 m/min
      339 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
      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 KAL-2

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
8.8
88.7
8820
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
19.6
925
Wingspan (Beam) (m)
0.1
 
11.9
95
Wing loading (kg/m2)
3.1
 
81.5
829
Aspect ratio
1.7
 
7.2
25.6
Rotors
Rotor number (qt)
1
 
1
8
Weights
Empty weight (kg)
8
 
1,110
276,800
Loaded weight (kg)
5
 
16,000
242,500
Speeds
Ground Speed (km/h)
96.6
 
293
1,500
Сruise Speed (km/h)
52
 
210
3,087
40% powerat 2135 m
Fuel
Fuel Capacity (l)
23
 
300
320,000
Power
Power/mass (hp/kg)
0.0
 
0.1
22.1
Total Power (hp)
0.4
 
240
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,500
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
282
36,000
Propellers
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 25.11.1954

Similar aircraft

Get more

Comments