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    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      7 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      21 m2
      32 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      57 kg/m2
      87 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
      1056 kg
      1584 kg
    • Max. takeoff weight (Gross weight)
      1520 kg
      2280 kg
    • Loaded weight
      5 kg
      242500 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
      240 km/h
      362 km/h
    • Сruise Speed
      148 km/h
      224 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
      504 hp
      757 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5816 m
      8724 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      723 km
      1085 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
      160 m/min
      240 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      8 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
      3 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
      604 qt
      906 qt
    • Price
      41 USD
      750000000 USD

Nakajima E8N

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.8
88.7
Height (m)
0.6
 
8.8
50.1
Wings
Wing area (m2)
1.1
 
26.5
925
Wingspan (Beam) (m)
0.1
 
11.0
95
Wing loading (kg/m2)
3.1
 
71.7
829
Weights
Empty weight (kg)
8
 
1,320
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,900
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
301
28,165
Сruise Speed (km/h)
52
 
186
3,087
Power
Total Power (hp)
0.4
 
630.0
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,270
161,544
Range (Ferry range) (km)
4
 
904
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
200
36,000
Time to altitude (min)
0.6
 
6.5
105
to 3000 m
Combat
Guns (qt)
1
 
2
18
7.7 mm (.303 in) machine guns
Bombs (qt)
1
 
2
250
30 kg (66 lb) bombs
Stat
Number built (qt)
0
 
755
43,000
Introduction 1934
First flight 01.03.1934

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