Search filter

    • Year
      1906
      2018
    • Length
      4 m
      8 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      22 m2
    • Wingspan (Beam)
      7 m
      12 m
    • Wing loading
      175 kg/m2
      264 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
      1156 kg
      1734 kg
    • Max. takeoff weight (Gross weight)
      3096 kg
      4644 kg
    • Loaded weight
      2400 kg
      3600 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
      720 km/h
      1080 km/h
    • Сruise Speed
      559 km/h
      839 km/h
    • Stall Speed
      120 km/h
      180 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      13 kN
      21 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
      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
      2400 m/min
      3600 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      3 min
      5 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
      5 qt
      9 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi J8M

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Integrated

Monoplane

Geometry
Length (m)
1.9
 
6.0
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
17.7
925
Wingspan (Beam) (m)
0.1
 
9.5
95
Wing loading (kg/m2)
3.1
 
219.2
829
Weights
Empty weight (kg)
8
 
1,445
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,870
575,000
Loaded weight (kg)
5
 
3,000
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
900
28,165
at 10000 m
Сruise Speed (km/h)
52
 
699
3,087
Stall Speed (km/h)
40
 
150
257.7
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Thrust (kN)
1.5
 
17.5
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
3,000
36,000
Time to altitude (min)
0.6
 
0.7
105
to 2000 m
0.6
 
2.1
105
to 4000 m
0.6
 
3.1
105
to 8000 m
0.6
 
3.8
105
to 10000 m
Combat
Guns (qt)
1
 
2
18
Type 5 30mm cannon with 53 rounds per gun
Stat
Number built (qt)
0
 
7
43,000
Introduction 1945
First flight 07.07.1945

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