Search filter

    • Year
      1906
      2018
    • Length
      5 m
      8 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      28 m2
    • Wingspan (Beam)
      8 m
      12 m
    • Wing loading
      61 kg/m2
      93 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
      1020 kg
      1532 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1408 kg
      2112 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
      281 km/h
      423 km/h
    • Сruise Speed
      228 km/h
      344 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
      584 hp
      877 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6192 m
      9288 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      677 km
      1017 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      2 h
      5 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
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      2 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
      176 qt
      266 qt
    • Price
      41 USD
      750000000 USD

Nakajima A4N

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.6
88.7
Height (m)
0.6
 
3.1
50.1
Wings
Wing area (m2)
1.1
 
22.9
925
Wingspan (Beam) (m)
0.1
 
10
95
Wing loading (kg/m2)
3.1
 
76.9
829
Weights
Empty weight (kg)
8
 
1,276
276,800
Loaded weight (kg)
5
 
1,760
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
352
28,165
at 3200 m
Сruise Speed (km/h)
52
 
286
3,087
Power
Total Power (hp)
0.4
 
730.6
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,740
161,544
Range (Ferry range) (km)
4
 
847
40,700
Endurance (h)
0.0
 
3.5
150
Dynamic Performance
Time to altitude (min)
0.6
 
3.5
105
to 3000 m
Combat
Guns (qt)
1
 
2
18
fixed, forward-firing 7.7 mm machine guns
Stat
Number built (qt)
0
 
221
43,000
Introduction 1936
First flight 01.09.1934

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