Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      37 m2
      57 m2
    • Wingspan (Beam)
      10 m
      17 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
      1288 kg
      1932 kg
    • Max. takeoff weight (Gross weight)
      2080 kg
      3120 kg
    • Loaded weight
      1880 kg
      2820 kg
    • Crew
      2 per.
      4 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
      131 km/h
      197 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      90 km/h
      136 km/h
    • Stall Speed
      67 km/h
      101 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
      280 hp
      420 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 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
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      48 min
      73 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      2 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
      4 qt
      8 qt
    • Price
      41 USD
      750000000 USD

Aichi AB-4

TypeAircraft
Company

Aichi Kokuki KK

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.8
88.7
Height (m)
0.6
 
3.9
50.1
Wings
Wing area (m2)
1.1
 
47.1
925
Wingspan (Beam) (m)
0.1
 
13.5
95
Weights
Empty weight (kg)
8
 
1,610
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,600
575,000
when catapulted
Loaded weight (kg)
5
 
2,350
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
164
1,500
Сruise Speed (km/h)
52
 
113
3,087
Stall Speed (km/h)
40
 
84
257.7
at 1000 m
Power
Total Power (hp)
0.4
 
349.9
60,000
0.4
 
350
60,000
1 powerplant
Dynamic Performance
Time to altitude (min)
0.6
 
60.8
105
Combat
Guns (qt)
1
 
1
18
7.7 mm (0.303 in) machine gun
Stat
Number built (qt)
0
 
6
43,000
Introduction 1932
First flight 01.05.1932

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