Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      19 m2
      29 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      93 kg/m2
      141 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
      1498 kg
      2248 kg
    • Max. takeoff weight (Gross weight)
      2336 kg
      3504 kg
    • Loaded weight
      2238 kg
      3358 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
      339 km/h
      509 km/h
    • Сruise Speed
      256 km/h
      384 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
      760 hp
      1141 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6616 m
      9924 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      848 km
      1272 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
      404 m/min
      606 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      7 min
      12 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      200 kg
      300 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1908 qt
      2862 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi Ki-51

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
9.2
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
24.0
925
Wingspan (Beam) (m)
0.1
 
12.1
95
Wing loading (kg/m2)
3.1
 
117
829
Weights
Empty weight (kg)
8
 
1,873
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,920
575,000
Loaded weight (kg)
5
 
2,798
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
424
28,165
at 3000 m
Сruise Speed (km/h)
52
 
320
3,087
Power
Total Power (hp)
0.4
 
950.4
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,270
161,544
Range (Ferry range) (km)
4
 
1,060
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
505
36,000
Time to altitude (min)
0.6
 
9.9
105
to 6000 m
Combat
Guns (qt)
1
 
3
18
2× fixed, forward-firing 7.7 mm (.303 in) Type 89 machine guns (replaced with 2× 12.7 mm (.5 in) Ho-103 machine guns in later models); 1× 7.7 mm (.303 in) Te-4 Machine gun rearward-firing machine gun.
Bombs weight (kg)
2
 
200
39,000
normal operations
2
 
250
39,000
for suicide operations
Stat
Number built (qt)
0
 
2,385
43,000
Introduction 1936
First flight 1939

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