Search filter

    • Year
      1906
      2018
    • Length
      9 m
      14 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      21 m2
      33 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      119 kg/m2
      180 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
      2640 kg
      3962 kg
    • Max. takeoff weight (Gross weight)
      3556 kg
      5334 kg
    • Loaded weight
      5 kg
      242500 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
      344 km/h
      516 km/h
    • Max. Speed
      379 km/h
      569 km/h
    • Сruise Speed
      236 km/h
      356 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
      1119 hp
      1680 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7920 m
      11880 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      952 km
      1428 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
      416 m/min
      624 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
      2 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      2 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      23 qt
      35 qt
    • Price
      41 USD
      750000000 USD

Aichi M6A

TypeAircraft
Company

Aichi Kokuki KK

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.6
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
27
925
Wingspan (Beam) (m)
0.1
 
12.3
95
Wing loading (kg/m2)
3.1
 
149.6
829
Weights
Empty weight (kg)
8
 
3,301
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,445
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
430
1,500
Max. Speed (km/h)
25
 
474
28,165
at 5200 m
Сruise Speed (km/h)
52
 
296
3,087
at 3000 m
Power
Total Power (hp)
0.4
 
1,399.5
60,000
Performance
Service ceiling (m)
0.6
 
9,900
161,544
Range (Ferry range) (km)
4
 
1,190
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
520
36,000
Combat
Guns (qt)
1
 
1
18
13 mm cabin-mounted Type 2 machine gun
Bombs (qt)
1
 
2
250
250 kg or
1
 
1
250
850 kg or
Torpedoes (qt)
1
 
1
4
Type 91 torpedo
Stat
Number built (qt)
0
 
29
43,000
Introduction 1943
First flight 1943
Stop production 1945

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