Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      20 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      253 kg/m2
      381 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
      2746 kg
      4120 kg
    • Max. takeoff weight (Gross weight)
      4200 kg
      6300 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      9 per.
      15 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      437 km/h
      657 km/h
    • Сruise Speed
      386 km/h
      580 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
      848 l
      1272 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
      1241 hp
      1863 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7216 m
      10824 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1867 km
      2801 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
      643 m/min
      965 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
      18 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
      563 qt
      845 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi MU-2

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
12.0
88.7
Height (m)
0.6
 
4.2
50.1
Wings
Wing area (m2)
1.1
 
16.6
925
Wingspan (Beam) (m)
0.1
 
11.9
95
Wing loading (kg/m2)
3.1
 
317
829
Weights
Empty weight (kg)
8
 
3,433
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,250
575,000
Capacity
Crew (per.)
1
 
1
112
1 or 2 pilots
Capacity passengers (per.)
1
 
12
400
4-12 passengers
Speeds
Max. Speed (km/h)
25
 
547
28,165
at 4575 m
Сruise Speed (km/h)
52
 
483
3,087
at 7620 m (econ cruise)
Fuel
Fuel Capacity (l)
23
 
1,060
320,000
Power
Total Power (hp)
0.4
 
1,552
60,000
2 powerplants 776 hp each
Performance
Service ceiling (m)
0.6
 
9,020
161,544
Range (Ferry range) (km)
4
 
2,334
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
804
36,000
Stat
Number built (qt)
0
 
704
43,000
Introduction 1963
First flight 14.09.1963

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