Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      10 m
      16 m
    • Wing loading
      54 kg/m2
      82 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
      848 kg
      1272 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1416 kg
      2124 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
      176 km/h
      266 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
      380 hp
      570 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4560 m
      6840 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
      4 h
      6 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
      8 min
      13 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      187 qt
      281 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi 2MR8

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
8.5
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
12.8
95
Wing loading (kg/m2)
3.1
 
68.1
829
Weights
Empty weight (kg)
8
 
1,060
276,800
Loaded weight (kg)
5
 
1,770
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
221
28,165
Power
Total Power (hp)
0.4
 
475
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,700
161,544
Endurance (h)
0.0
 
5
150
4-5 hours
Dynamic Performance
Time to altitude (min)
0.6
 
10.5
105
to 3000 m
Combat
Guns (qt)
1
 
4
18
2 × fixed forward firing 7.7 mm (.303 in) machine guns, 2 × flexibly mounted machine guns in rear cockpit
Stat
Number built (qt)
0
 
234
43,000
4 prototypes + 230 production aircraft
Introduction 1930
First flight 28.03.1931

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