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    • Year
      1906
      2018
    • Length
      23 m
      36 m
    • Height
      7 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      74 m2
      112 m2
    • Wingspan (Beam)
      24 m
      38 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
      15422 kg
      23134 kg
    • Max. takeoff weight (Gross weight)
      27216 kg
      40824 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      9 per.
      15 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
      520 km/h
      780 km/h
    • Сruise Speed
      321 km/h
      483 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
      10356 l
      15536 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
      4560 hp
      6840 hp
    • Thrust
      21 kN
      33 kN
    • Service ceiling
      7320 m
      10980 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3556 km
      5334 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
      438 m/min
      658 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      3 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      2 qt
      4 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
      2903 kg
      4355 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      66 qt
      100 qt
    • Price
      41 USD
      750000000 USD

Kawasaki P-2J

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
29.2
88.7
Height (m)
0.6
 
8.9
50.1
Wings
Wing area (m2)
1.1
 
92.9
925
Wingspan (Beam) (m)
0.1
 
30.9
95
Weights
Empty weight (kg)
8
 
19,278
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
34,020
575,000
Capacity
Crew (per.)
1
 
12
112
2 pilots + 10 operators
Speeds
Max. Speed (km/h)
25
 
650
28,165
Сruise Speed (km/h)
52
 
402
3,087
Fuel
Fuel Capacity (l)
23
 
12,946
320,000
Power
Total Power (hp)
0.4
 
5,700
60,000
2 powerplants 2850 hp each
Thrust (kN)
1.5
 
27.4
1,914
2 powerplants 13,7 kN each
Performance
Service ceiling (m)
0.6
 
9,150
161,544
Range (Ferry range) (km)
4
 
4,445
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
548
36,000
Propellers
Propellers (qt)
1
 
2
8
Prop blade number (qt)
1
 
3
8
Combat
Bombs weight (kg)
2
 
3,629
39,000
including free-fall bombs, depth charges, and torpedoes
Stat
Number built (qt)
0
 
83
43,000
Introduction 1966
First flight 21.07.1966
Stop production 1996

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