Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      10 m
      16 m
    • Wing loading
      3 kg/m2
      829 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
      3646 kg
      5471 kg
    • Max. takeoff weight (Gross weight)
      5842 kg
      8764 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      2122 kg
      3184 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      7 per.
      11 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      692 km/h
      1040 km/h
    • Сruise Speed
      656 km/h
      984 km/h
    • Stall Speed
      136 km/h
      206 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
      0 hp
      60000 hp
    • Thrust
      20 kN
      31 kN
    • Service ceiling
      10972 m
      16460 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2508 km
      3762 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
      919 m/min
      1379 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
      80 qt
      120 qt
    • Price
      5920000 USD
      8880000 USD

Mitsubishi Mu-300

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
14.8
88.7
Height (m)
0.6
 
4.2
50.1
Wings
Wing area (m2)
1.1
 
22.4
925
Wingspan (Beam) (m)
0.1
 
13.3
95
Weights
Empty weight (kg)
8
 
4,558.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,302.8
575,000
Capacity
Crew (per.)
1
 
2
112
pilots
Useful load (kg)
26.4
 
2,653
90,700
Capacity passengers (per.)
1
 
9
400
7—9 passengers
Speeds
Max. Speed (km/h)
25
 
866
28,165
Сruise Speed (km/h)
52
 
820
3,087
at 7000 m
Stall Speed (km/h)
40
 
171
257.7
full flaps
Power
Thrust (kN)
1.5
 
25.8
1,914
2 powerplants 12,9 kN
Performance
Service ceiling (m)
0.6
 
13,716
161,544
Range (Ferry range) (km)
4
 
3,135
40,700
at 13700 m
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,149.1
36,000
Stat
Number built (qt)
0
 
100
43,000
Price (USD)
41.5
 
7.4 million
750.0 million
Introduction 1978
First flight 29.08.1978

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