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    • Year
      1906
      2018
    • Length
      35 m
      54 m
    • Height
      7 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      281 m2
      423 m2
    • Wingspan (Beam)
      51 m
      78 m
    • Wing loading
      365 kg/m2
      549 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      9
      15
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      4 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
      52000 kg
      78000 kg
    • Max. takeoff weight (Gross weight)
      128000 kg
      192000 kg
    • Loaded weight
      97600 kg
      146400 kg
    • Crew
      1 per.
      112 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
      543 km/h
      815 km/h
    • Сruise Speed
      52 km/h
      3087 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
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      12000 m
      18000 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
      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
      1 m/min
      36000 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
      3 m
      6 m
    • Prop blade number
      4 qt
      8 qt
    • Guns
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      16000 kg
      24000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Nakajima G10N

Company

Nakajima Aircraft Company

Scheme

Monoplane

Geometry
Length (m)
1.9
 
45.0
88.7
Height (m)
0.6
 
8.8
50.1
Wings
Wing area (m2)
1.1
 
352.0
925
Wingspan (Beam) (m)
0.1
 
65.0
95
Wing loading (kg/m2)
3.1
 
457.0
829
3.1
 
457.0
829
Aspect ratio
1.7
 
12.1
25.6
Rotors
Rotor number (qt)
1
 
6
8
Weights
Empty weight (kg)
8
 
65,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
160,000
575,000
Loaded weight (kg)
5
 
122,000
242,500
Speeds
Max. Speed (km/h)
25
 
679
28,165
at 10000 m
Power
Power/mass (hp/kg)
0.0
 
0.1
22.1
Performance
Service ceiling (m)
0.6
 
15,000
161,544
Propellers
Prop diameter (m)
1.8
 
4.8
5.8
Prop blade number (qt)
1
 
6
8
Combat
Guns (qt)
1
 
4
18
20mm Type 99 cannon
Bombs weight (kg)
2
 
20,000
39,000
Stat

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