Search filter

    • Year
      1906
      2018
    • Length
      30 m
      46 m
    • Height
      9 m
      15 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      28 m
      43 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
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      63760 kg
      95640 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      17 per.
      27 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      6 qt
      10 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      796 km/h
      1196 km/h
    • Сruise Speed
      666 km/h
      1000 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
      23 l
      320000 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
      192 kN
      288 kN
    • Service ceiling
      10777 m
      16167 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      6400 km
      9600 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
      1 m/min
      36000 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
      7200 kg
      10800 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      133600000 USD
      200400000 USD

Kawasaki P-1

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
38
88.7
Height (m)
0.6
 
12.1
50.1
Wings
Wingspan (Beam) (m)
0.1
 
35.4
95
Weights
Max. takeoff weight (Gross weight) (kg)
154
 
79,700
575,000
Capacity
Crew (per.)
1
 
22
112
Flight: 2 Mission: 11
Hardpoints (qt)
1
 
8
2,576
Speeds
Max. Speed (km/h)
25
 
996
28,165
Сruise Speed (km/h)
52
 
833
3,087
Power
Thrust (kN)
1.5
 
240
1,914
4 powerplants 60 kN each
Performance
Service ceiling (m)
0.6
 
13,472.2
161,544
Range (Ferry range) (km)
4
 
8,000
40,700
Combat
Bombs weight (kg)
2
 
9,000
39,000
Stat
Price (USD)
41.5
 
167.0 million
750.0 million
Introduction 2013
First flight 28.09.2007

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