Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 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
      84 m2
      127 m2
    • Main rotor diameter
      9 m
      14 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
      1960 kg
      2940 kg
    • Max. takeoff weight (Gross weight)
      3200 kg
      4800 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
      3 qt
      5 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      222 km/h
      334 km/h
    • Сruise Speed
      176 km/h
      264 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
      1424 hp
      2136 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3904 m
      5856 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      440 km
      660 km
    • Range PTB (Ferry range)
      720 km
      864 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      30 qt
      46 qt
    • Price
      41 USD
      750000000 USD

Kawasaki OH-1

TypeHelicopter
Company

Kawasaki Heavy Industries

Geometry
Length (m)
1.9
 
12
88.7
Height (m)
0.6
 
3.8
50.1
Rotors
Disc area (m2)
1.4
 
105.7
460
Main rotor diameter (m)
1.2
 
11.6
62
Weights
Empty weight (kg)
8
 
2,450
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,000
575,000
Capacity
Crew (per.)
1
 
2
112
pilot and observer
Hardpoints (qt)
1
 
4
2,576
pylons for rockets, gun pods, anti-tank missiles, or Type 91 air-to-air missiles
Speeds
Max. Speed (km/h)
25
 
278
28,165
Сruise Speed (km/h)
52
 
220
3,087
Power
Total Power (hp)
0.4
 
1,780
60,000
2 powerplants 890 hp each
Performance
Service ceiling (m)
0.6
 
4,880
161,544
Range (Ferry range) (km)
4
 
550
40,700
Range PTB (Ferry range) (km)
720
 
720
10,000
Stat
Number built (qt)
0
 
38
43,000
Introduction 2000
First flight 06.08.1996

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