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    • Year
      1906
      2018
    • Length
      24 m
      38 m
    • Height
      7 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      161 m2
      243 m2
    • Wingspan (Beam)
      33 m
      51 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
      16080 kg
      24120 kg
    • Max. takeoff weight (Gross weight)
      25600 kg
      38400 kg
    • Loaded weight
      22520 kg
      33780 kg
    • Crew
      5 per.
      9 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
      336 km/h
      504 km/h
    • Сruise Speed
      222 km/h
      334 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
      5984 hp
      8976 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5960 m
      8940 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3408 km
      5112 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
      756 m/min
      1134 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
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      3200 kg
      4800 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Nakajima G5N

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
31.0
88.7
Height (m)
0.6
 
8.8
50.1
Wings
Wing area (m2)
1.1
 
201.8
925
Wingspan (Beam) (m)
0.1
 
42.1
95
Weights
Empty weight (kg)
8
 
20,100
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
32,000
575,000
Loaded weight (kg)
5
 
28,150
242,500
Capacity
Crew (per.)
1
 
7
112
Speeds
Max. Speed (km/h)
25
 
420
28,165
Сruise Speed (km/h)
52
 
278
3,087
Power
Total Power (hp)
0.4
 
7,480
60,000
4 powerplants 1870 hp each
Performance
Service ceiling (m)
0.6
 
7,450
161,544
Range (Ferry range) (km)
4
 
4,260
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
945
36,000
Combat
Guns (qt)
1
 
6
18
2× 20 mm Type 99 cannons; 4× 7.7 mm (0.303 in) Type 92 machine guns
Bombs weight (kg)
2
 
4,000
39,000
bombs or torpedoes
Stat
Introduction 1941
First flight 08.04.1941
Stop production 1945

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