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
      37 m2
      56 m2
    • Wingspan (Beam)
      11 m
      18 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
      1541 kg
      2313 kg
    • Max. takeoff weight (Gross weight)
      2637 kg
      3957 kg
    • Loaded weight
      5 kg
      242500 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
      96 km/h
      1500 km/h
    • Max. Speed
      173 km/h
      261 km/h
    • Сruise Speed
      108 km/h
      162 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
      496 hp
      744 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3540 m
      5310 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1650 km
      2476 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
      132 m/min
      198 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
      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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Aichi E11A

TypeAircraft
Company

Aichi Kokuki KK

Scheme

Biplane

Geometry
Length (m)
1.9
 
10.7
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
46.4
925
Wingspan (Beam) (m)
0.1
 
14.5
95
Weights
Empty weight (kg)
8
 
1,927
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,297
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
217
28,165
Сruise Speed (km/h)
52
 
135
3,087
Power
Total Power (hp)
0.4
 
620
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,425
161,544
Range (Ferry range) (km)
4
 
2,063
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
165
36,000
Combat
Guns (qt)
1
 
1
18
7.7 mm (.303 in) Type 92 machine gun
Stat
Introduction 1937

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