Search filter

    • Year
      1906
      2018
    • Length
      9 m
      14 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      28 m2
      43 m2
    • Wingspan (Beam)
      11 m
      18 m
    • Wing loading
      127 kg/m2
      191 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
      3048 kg
      4572 kg
    • Max. takeoff weight (Gross weight)
      5200 kg
      7800 kg
    • Loaded weight
      4500 kg
      6750 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
      453 km/h
      681 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
      1458 hp
      2188 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9000 m
      13500 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2430 km
      3646 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1440 km
      2160 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
      460 m/min
      692 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
      2 qt
    • Bombs weight
      640 kg
      960 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      91 qt
      137 qt
    • Price
      41 USD
      750000000 USD

Aichi B7A

TypeAircraft
Company

Aichi Kokuki KK

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.5
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
35.4
925
Wingspan (Beam) (m)
0.1
 
14.4
95
Wing loading (kg/m2)
3.1
 
158.9
829
Weights
Empty weight (kg)
8
 
3,810
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,500
575,000
Loaded weight (kg)
5
 
5,625
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
567
28,165
Power
Total Power (hp)
0.4
 
1,823.1
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
11,250
161,544
Range (Ferry range) (km)
4
 
3,038
40,700
Сombat radius (km)
277
 
1,800
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
576
36,000
Combat
Guns (qt)
1
 
3
18
2× 20 mm Type 99 Model 2 cannons in wings; 1× 7.92 mm (0.312 in) Type 1 or 13 mm (0.51 in) Type 2 machine gun in the rear cockpit
Torpedoes (qt)
1
 
1
4
800 kg (1,764 lb) torpedo
Bombs weight (kg)
2
 
800
39,000
of general ordnance or
Stat
Number built (qt)
0
 
114
43,000
Introduction 1942
First flight 01.05.1942
Stop production 01.09.1945

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