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
      14 m2
      23 m2
    • Wingspan (Beam)
      9 m
      14 m
    • Wing loading
      66 kg/m2
      101 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
      888 kg
      1332 kg
    • Max. takeoff weight (Gross weight)
      1432 kg
      2148 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 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
      376 km/h
      564 km/h
    • Max. Speed
      376 km/h
      564 km/h
    • Сruise Speed
      280 km/h
      420 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
      520 hp
      781 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9800 m
      14700 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      501 km
      753 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      501 km
      753 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
      734 m/min
      1102 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
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      80 kg
      120 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      2694 qt
      4042 qt
    • Price
      41 USD
      750000000 USD

Nakajima Ki-27

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
7.5
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
18.6
925
Wingspan (Beam) (m)
0.1
 
11.3
95
Wing loading (kg/m2)
3.1
 
83.4
829
Weights
Empty weight (kg)
8
 
1,110
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,790
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
470
1,500
Max. Speed (km/h)
25
 
470
28,165
Сruise Speed (km/h)
52
 
350
3,087
Power
Total Power (hp)
0.4
 
650.1
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
12,250
161,544
Range (Ferry range) (km)
4
 
627
40,700
Сombat radius (km)
277
 
627
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
918
36,000
Combat
Guns (qt)
1
 
2
18
7.7 mm Type 89 machine guns
Bombs weight (kg)
2
 
100
39,000
Stat
Number built (qt)
0
 
3,368
43,000
Introduction 1936
First flight 15.10.1936
Stop production 1945

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