Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      28 kg/m2
      42 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
      784 kg
      1176 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1056 kg
      1584 kg
    • Crew
      1 per.
      3 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
      163 km/h
      245 km/h
    • Сruise Speed
      52 km/h
      3087 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
      240 hp
      361 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 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
      2 h
      4 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
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      13 min
      21 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
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      24 kg
      36 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      127 qt
      191 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi 2MR

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.9
88.7
Height (m)
0.6
 
2.9
50.1
Wings
Wingspan (Beam) (m)
0.1
 
12.0
95
Wing loading (kg/m2)
3.1
 
35
829
Weights
Empty weight (kg)
8
 
980
276,800
Loaded weight (kg)
5
 
1,320
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
204
28,165
Power
Total Power (hp)
0.4
 
300.3
60,000
1 powerplant
Performance
Endurance (h)
0.0
 
3
150
Dynamic Performance
Time to altitude (min)
0.6
 
17
105
to 3000 m
Combat
Guns (qt)
1
 
4
18
2 fixed forward firing 7.7 mm machine guns and 2 flexibly mounted 7.7 mm machine guns in observers cockpit
Bombs weight (kg)
2
 
30
39,000
of bombs
Stat
Number built (qt)
0
 
159
43,000
Introduction 1922
First flight 12.01.1922

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