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    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      32 m2
      48 m2
    • Wingspan (Beam)
      13 m
      21 m
    • Wing loading
      140 kg/m2
      211 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
      3584 kg
      5376 kg
    • Max. takeoff weight (Gross weight)
      6547 kg
      9821 kg
    • Loaded weight
      5608 kg
      8412 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
      405 km/h
      609 km/h
    • Сruise Speed
      266 km/h
      400 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
      1360 l
      2040 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1568 hp
      2352 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7456 m
      11184 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2036 km
      3054 km
    • Range PTB (Ferry range)
      3022 km
      4534 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
      417 m/min
      627 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      7 min
      12 min
    • Propellers
      1 qt
      3 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      2 qt
      4 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      383 qt
      575 qt
    • Price
      41 USD
      750000000 USD

Nakajima J1N

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
12.8
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
40
925
Wingspan (Beam) (m)
0.1
 
17.0
95
Wing loading (kg/m2)
3.1
 
175.3
829
Weights
Empty weight (kg)
8
 
4,480
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,184
575,000
Loaded weight (kg)
5
 
7,010
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
507
28,165
Сruise Speed (km/h)
52
 
333
3,087
at 4000 m
Fuel
Fuel Capacity (l)
23
 
1,700
320,000
Power
Power/mass (hp/kg)
0.0
 
0.4
22.1
Total Power (hp)
0.4
 
2,260
60,000
2 powerplants take-off rating
0.4
 
2,200
60,000
2 powerplants at (2850 m)
0.4
 
1,960
60,000
2 powerplants (at 6000m)
Performance
Service ceiling (m)
0.6
 
9,320
161,544
Range (Ferry range) (km)
4
 
2,545
40,700
Range PTB (Ferry range) (km)
720
 
3,778.1
10,000
Dynamic Performance
Rate of climb (m/min)
1.9
 
522
36,000
Time to altitude (min)
0.6
 
9.6
105
to 5000 m
Propellers
Propellers (qt)
1
 
2
8
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
4
18
20 mm Type 99 cannon, two upward- and two downward-firing or
1
 
2
18
20 mm Type 99 cannon, firing upward only or
1
 
3
18
20 mm Type 99 cannon, all three firing upward
Stat
Number built (qt)
0
 
479
43,000
Introduction 1942
First flight 01.05.1941
Stop production 1945

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