Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      22 m2
    • Wingspan (Beam)
      8 m
      14 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
      972 kg
      1460 kg
    • Max. takeoff weight (Gross weight)
      1457 kg
      2187 kg
    • Loaded weight
      1364 kg
      2046 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
      352 km/h
      528 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
      628 hp
      942 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7840 m
      11760 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      960 km
      1440 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
      615 m/min
      923 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
      3 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
      875 qt
      1313 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi A5M

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
7.6
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
17.8
925
Wingspan (Beam) (m)
0.1
 
11
95
Weights
Empty weight (kg)
8
 
1,216
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,822
575,000
Loaded weight (kg)
5
 
1,705
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
440
28,165
at 3000 m
Power
Total Power (hp)
0.4
 
785
60,000
1 powerplant at 3000 m
Performance
Service ceiling (m)
0.6
 
9,800
161,544
Range (Ferry range) (km)
4
 
1,200
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
769
36,000
Combat
Guns (qt)
1
 
2
18
7.7 mm Type 89 machine gun (0.303 in) fuselage-mounted machine guns
Stat
Number built (qt)
0
 
1,094
43,000
Introduction 1935
First flight 04.02.1935
Stop production 1945

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