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
      22 m2
      34 m2
    • Wingspan (Beam)
      10 m
      16 m
    • Wing loading
      111 kg/m2
      168 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
      2356 kg
      3534 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      3642 kg
      5464 kg
    • Crew
      1 per.
      3 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
      351 km/h
      527 km/h
    • Сruise Speed
      281 km/h
      423 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
      1040 hp
      1561 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8000 m
      12000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1936 km
      2904 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
      480 m/min
      720 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
      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
      200 kg
      300 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      204 qt
      308 qt
    • Price
      41 USD
      750000000 USD

Aichi E16A

TypeAircraft
Company

Aichi Kokuki KK

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
10.8
88.7
Height (m)
0.6
 
4.8
50.1
Wings
Wing area (m2)
1.1
 
28
925
Wingspan (Beam) (m)
0.1
 
12.8
95
Wing loading (kg/m2)
3.1
 
139.3
829
Weights
Empty weight (kg)
8
 
2,945
276,800
Loaded weight (kg)
5
 
4,553
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and observer
Speeds
Max. Speed (km/h)
25
 
439
28,165
Сruise Speed (km/h)
52
 
352
3,087
Power
Total Power (hp)
0.4
 
1,300.3
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
10,000
161,544
Range (Ferry range) (km)
4
 
2,420
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
600
36,000
Combat
Guns (qt)
1
 
3
18
2 fixed forward-firing 20 mm Type 99 cannons in wings; 1 flexible rearward-firing 13 mm (.51 in) Type 2 machine gun for observer
Bombs weight (kg)
2
 
250
39,000
Stat
Number built (qt)
0
 
256
43,000
Introduction 1942
First flight 22.05.1942

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