Search filter

    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      24 m2
    • Wingspan (Beam)
      8 m
      14 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
      860 kg
      1290 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1224 kg
      1836 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
      96 km/h
      1500 km/h
    • Max. Speed
      240 km/h
      360 km/h
    • Сruise Speed
      214 km/h
      322 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
      416 hp
      625 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7200 m
      10800 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
      1 h
      3 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
      600 m/min
      900 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      3 min
      5 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      360 qt
      540 qt
    • Price
      41 USD
      750000000 USD

Nakajima Army Type 91 Fighter

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Parasol

Monoplane

Geometry
Length (m)
1.9
 
7.3
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
20
925
Wingspan (Beam) (m)
0.1
 
11
95
Weights
Empty weight (kg)
8
 
1,075
276,800
Loaded weight (kg)
5
 
1,530
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
300
28,165
Сruise Speed (km/h)
52
 
268
3,087
Power
Total Power (hp)
0.4
 
520.1
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
9,000
161,544
Endurance (h)
0.0
 
2
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
750
36,000
Time to altitude (min)
0.6
 
4
105
to 3000 m
Combat
Guns (qt)
1
 
2
18
fixed, forward-firing 7.7 mm (.303 in) machine guns
Stat
Number built (qt)
0
 
450
43,000
Introduction 1931
First flight 1931
Stop production 1937

Similar aircraft

Get more

Comments