Search filter

    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      60 m2
      90 m2
    • Wingspan (Beam)
      20 m
      30 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
      3972 kg
      5958 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      6400 kg
      9600 kg
    • Crew
      5 per.
      9 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
      300 km/h
      450 km/h
    • Сruise Speed
      224 km/h
      336 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
      3099 l
      4649 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
      1697 hp
      2547 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7360 m
      11040 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3520 km
      5280 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
      288 m/min
      432 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
      4 qt
      6 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
      838 qt
      1258 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi G3M

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
16.5
88.7
Height (m)
0.6
 
3.7
50.1
Wings
Wing area (m2)
1.1
 
75
925
Wingspan (Beam) (m)
0.1
 
25
95
Weights
Empty weight (kg)
8
 
4,965
276,800
Loaded weight (kg)
5
 
8,000
242,500
Capacity
Crew (per.)
1
 
7
112
Speeds
Max. Speed (km/h)
25
 
375
28,165
Сruise Speed (km/h)
52
 
280
3,087
Fuel
Fuel Capacity (l)
23
 
3,874
320,000
Power
Total Power (hp)
0.4
 
2,122
60,000
2 powerplants 1061 h each
Performance
Service ceiling (m)
0.6
 
9,200
161,544
Range (Ferry range) (km)
4
 
4,400
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
360
36,000
Combat
Guns (qt)
1
 
5
18
1× 20 mm (0.79 in) Type 99 cannon in rear dorsal turret; 4× 7.7 mm (0.30 in) Type 92 machine gun in cockpit, left and right side positions, and in retractable forward dorsal turret.
Torpedoes (qt)
1
 
1
4
aerial torpedo
Bombs weight (kg)
2
 
800
39,000
of bombs or
Stat
Number built (qt)
0
 
1,048
43,000
Introduction 1943
First flight 01.07.1935
Stop production 1945

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