Search filter

    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      24 m2
      38 m2
    • Wingspan (Beam)
      11 m
      17 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
      2580 kg
      3872 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      3776 kg
      5664 kg
    • Crew
      1 per.
      2 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
      504 km/h
      756 km/h
    • Сruise Speed
      333 km/h
      501 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
      1760 hp
      2640 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8720 m
      13080 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      992 km
      1488 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      2 h
      4 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
      788 m/min
      1182 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      4 min
      8 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      3 qt
      5 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
      7 qt
      11 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi A7M

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.0
88.7
Height (m)
0.6
 
4.3
50.1
Wings
Wing area (m2)
1.1
 
30.9
925
Wingspan (Beam) (m)
0.1
 
14
95
Weights
Empty weight (kg)
8
 
3,226
276,800
Loaded weight (kg)
5
 
4,720
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
630
28,165
at 6600 m
Сruise Speed (km/h)
52
 
417
3,087
Power
Total Power (hp)
0.4
 
2,200
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
10,900
161,544
Range (Ferry range) (km)
4
 
1,240
40,700
Endurance (h)
0.0
 
3
150
2.5 hr cruise + 30 min combat
Dynamic Performance
Rate of climb (m/min)
1.9
 
985
36,000
Time to altitude (min)
0.6
 
6.1
105
to 6000 m
Combat
Guns (qt)
1
 
4
18
2 × 13.2 mm Type 3 machine guns in the wings; 2 × 20 mm Type 99 cannons in the wings or
1
 
4
18
20 mm Type 99 cannons in the wings
Stat
Number built (qt)
0
 
9
43,000
Introduction 1944
First flight 06.05.1944

Similar aircraft

Get more

Comments