Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      25 m2
    • Wingspan (Beam)
      8 m
      13 m
    • Wing loading
      139 kg/m2
      209 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
      2271 kg
      3407 kg
    • Max. takeoff weight (Gross weight)
      2748 kg
      4122 kg
    • Loaded weight
      2568 kg
      3854 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
      524 km/h
      786 km/h
    • Сruise Speed
      280 km/h
      420 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
      1480 hp
      2220 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9144 m
      13716 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      448 km
      672 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
      1121 m/min
      1683 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
      3 qt
      5 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
      434 qt
      652 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi J2M

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
9.7
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
20.1
925
Wingspan (Beam) (m)
0.1
 
10.8
95
Wing loading (kg/m2)
3.1
 
174
829
Weights
Empty weight (kg)
8
 
2,839
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,435
575,000
Loaded weight (kg)
5
 
3,211
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
655
28,165
Сruise Speed (km/h)
52
 
350
3,087
Power
Total Power (hp)
0.4
 
1,850
60,000
1 poweplant
Performance
Service ceiling (m)
0.6
 
11,430
161,544
Range (Ferry range) (km)
4
 
560
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,402
36,000
Combat
Guns (qt)
1
 
4
18
20 mm Type 99-2 cannons in the wings
Bombs (qt)
1
 
2
250
2 × 60 kg (132 lb) bombs or 2 × 200 L (53 US gal) drop tanks.
Stat
Number built (qt)
0
 
543
43,000
Introduction 01.12.1942
First flight 20.03.1942
Stop production 01.08.1945

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