Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      159 kg/m2
      240 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
      2720 kg
      4080 kg
    • Max. takeoff weight (Gross weight)
      4204 kg
      6306 kg
    • Loaded weight
      3520 kg
      5280 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
      604 km/h
      908 km/h
    • Сruise Speed
      369 km/h
      555 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
      1520 hp
      2280 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      1 h
      3 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
      426 m/min
      641 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      12 min
      18 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      2 m
      4 m
    • Prop blade number
      4 qt
      8 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      1 qt
      3 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi J4M

Company

Mitsubishi Aircraft Corporation

Geometry
Length (m)
1.9
 
13.0
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wing area (m2)
1.1
 
22
925
Wingspan (Beam) (m)
0.1
 
12.5
95
Wing loading (kg/m2)
3.1
 
199.7
829
Weights
Empty weight (kg)
8
 
3,400
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,255
575,000
Loaded weight (kg)
5
 
4,400
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
756
28,165
at 8000 m
Сruise Speed (km/h)
52
 
462
3,087
Power
Total Power (hp)
0.4
 
2,100
60,000
1 powerplant at take-off
0.4
 
1,900
60,000
1powerplant at 2000 m
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Endurance (h)
0.0
 
2.2
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
533.4
36,000
Time to altitude (min)
0.6
 
15
105
to 8000 m
Propellers
Prop diameter (m)
1.8
 
3.2
5.8
Prop blade number (qt)
1
 
6
8
Combat
Guns (qt)
1
 
3
18
1x 30mm Type 5 cannon with 100 rounds + 2x 20mm Type 99 cannon with 200 rounds per gun in the fuselage nose
Bombs (qt)
1
 
2
250
60 kg (132 lb) bombs
Stat
Number built (qt)
0
 
1
43,000

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