Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      27 m2
      42 m2
    • Wingspan (Beam)
      9 m
      14 m
    • Wing loading
      57 kg/m2
      87 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
      1212 kg
      1820 kg
    • Max. takeoff weight (Gross weight)
      2088 kg
      3132 kg
    • Loaded weight
      2000 kg
      3000 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
      247 km/h
      371 km/h
    • Сruise Speed
      52 km/h
      3087 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
      584 hp
      876 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5584 m
      8376 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      741 km
      1113 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
      305 m/min
      459 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
      2 qt
      4 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
      472 qt
      708 qt
    • Price
      41 USD
      750000000 USD

Aichi D1A

TypeAircraft
Company

Aichi Kokuki KK

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.3
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
34.7
925
Wingspan (Beam) (m)
0.1
 
11.4
95
Wing loading (kg/m2)
3.1
 
72
829
Weights
Empty weight (kg)
8
 
1,516
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,610
575,000
Loaded weight (kg)
5
 
2,500
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and gunner
Speeds
Max. Speed (km/h)
25
 
309
28,165
Power
Total Power (hp)
0.4
 
730
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,980
161,544
Range (Ferry range) (km)
4
 
927
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
382.2
36,000
Combat
Guns (qt)
1
 
3
18
2× fixed 7.7 mm (.303 in) Type 92 machine guns; 1× flexible 7.7 mm (.303 in) Type 92 machine gun
Bombs (qt)
1
 
3
250
1× 250 kg (551 lb) bomb under fuselage; 2× 30 kg (66 lb) bombs under wings
Stat
Number built (qt)
0
 
590
43,000
Introduction 1934
First flight 1934
Stop production 1942

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