Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      38 m2
    • Wingspan (Beam)
      12 m
      20 m
    • Wing loading
      72 kg/m2
      110 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
      1472 kg
      2209 kg
    • Max. takeoff weight (Gross weight)
      2288 kg
      3432 kg
    • Loaded weight
      2286 kg
      3430 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      8 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      270 km/h
      406 km/h
    • Сruise Speed
      247 km/h
      371 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
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      552 hp
      828 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5486 m
      8230 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      836 km
      1256 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
      200 m/min
      300 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      6 min
      10 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
      8 qt
      14 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi Hinazuru

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
10.5
88.7
Height (m)
0.6
 
2.9
50.1
Wings
Wing area (m2)
1.1
 
31.5
925
Wingspan (Beam) (m)
0.1
 
15.9
95
Wing loading (kg/m2)
3.1
 
91
829
Weights
Empty weight (kg)
8
 
1,840.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,860
575,000
Loaded weight (kg)
5
 
2,857.6
242,500
Capacity
Crew (per.)
1
 
1
112
pilot
Capacity passengers (per.)
1
 
6
400
Speeds
Max. Speed (km/h)
25
 
338.0
28,165
at 2230 m
Сruise Speed (km/h)
52
 
309.0
3,087
at 75% power and 2230 m
Power
Power/mass (hp/kg)
0.0
 
0.2
22.1
Total Power (hp)
0.4
 
690
60,000
2 powerplants 345 hp each
Performance
Service ceiling (m)
0.6
 
6,858
161,544
Range (Ferry range) (km)
4
 
1,046
40,700
at 62.5% power and 3050 m
Dynamic Performance
Rate of climb (m/min)
1.9
 
250
36,000
Time to altitude (min)
0.6
 
8
105
to 3050 m
Stat
Number built (qt)
0
 
11
43,000
Introduction 1934
First flight 26.06.1934
Stop production 1951

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