Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      32 m2
      49 m2
    • Wingspan (Beam)
      10 m
      16 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
      1536 kg
      2304 kg
    • Max. takeoff weight (Gross weight)
      2640 kg
      3960 kg
    • Loaded weight
      2416 kg
      3624 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
      180 km/h
      271 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      118 km/h
      178 km/h
    • Stall Speed
      64 km/h
      98 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
      1 kN
      1914 kN
    • Service ceiling
      3880 m
      5820 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
      9 h
      15 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
      11 min
      18 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      2 qt
      4 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
      2 qt
    • Price
      41 USD
      750000000 USD

Aichi AB-6

Company

Aichi Kokuki KK

Scheme

Biplane

Geometry
Length (m)
1.9
 
10.4
88.7
Height (m)
0.6
 
4.8
50.1
Wings
Wing area (m2)
1.1
 
40.6
925
Wingspan (Beam) (m)
0.1
 
13.0
95
Weights
Empty weight (kg)
8
 
1,920
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,300
575,000
Loaded weight (kg)
5
 
3,020
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
225.3
1,500
Сruise Speed (km/h)
52
 
148
3,087
at 1000 m
Stall Speed (km/h)
40
 
81
257.7
Performance
Service ceiling (m)
0.6
 
4,850
161,544
Endurance (h)
0.0
 
11.9
150
Dynamic Performance
Time to altitude (min)
0.6
 
14.9
105
to 3000 m
Combat
Guns (qt)
1
 
3
18
1× fixed, forward firing 7.7 mm machine gun, 1 flexibly mounted in rear cockpit and 1× under fuselage
Stat
Number built (qt)
0
 
1
43,000
First flight 1933

Similar aircraft

Get more

Comments