Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      26 m2
    • Wingspan (Beam)
      7 m
      12 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
      3032 kg
      4548 kg
    • Max. takeoff weight (Gross weight)
      6000 kg
      9000 kg
    • Loaded weight
      5 kg
      242500 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
      3 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      830 km/h
      1246 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
      1792 l
      2690 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
      25 kN
      39 kN
    • Service ceiling
      12192 m
      18288 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1336 km
      2004 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1037 km
      1557 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
      5 G
      9 G
    • Rate of climb
      2438 m/min
      3658 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 T-4

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
13
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
21
925
Wingspan (Beam) (m)
0.1
 
9.9
95
Weights
Empty weight (kg)
8
 
3,790
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,500
575,000
Capacity
Crew (per.)
1
 
2
112
two pilots in tandem
Hardpoints (qt)
1
 
2
2,576
Speeds
Max. Speed (km/h)
25
 
1,038
28,165
Fuel
Fuel Capacity (l)
23
 
2,241
320,000
Power
Thrust (kN)
1.5
 
32
1,914
2 powerplants 16 kN each
Performance
Service ceiling (m)
0.6
 
15,240
161,544
Range (Ferry range) (km)
4
 
1,670
40,700
Сombat radius (km)
277
 
1,297
7,210
Dynamic Performance
Load factor from (G)
2
 
7.3
9
Rate of climb (m/min)
1.9
 
3,048
36,000
Stat
Introduction 1985
First flight 29.07.1985

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