Search filter

    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      27 m2
    • Wingspan (Beam)
      10 m
      15 m
    • Wing loading
      140 kg/m2
      212 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
      2374 kg
      3562 kg
    • Max. takeoff weight (Gross weight)
      4208 kg
      6312 kg
    • Loaded weight
      3600 kg
      5400 kg
    • Crew
      2 per.
      4 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
      488 km/h
      732 km/h
    • Сruise Speed
      309 km/h
      465 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
      1592 hp
      2389 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8376 m
      12564 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4240 km
      6360 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      2656 km
      3984 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
      588 m/min
      884 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      6 min
      10 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      2 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
      370 qt
      556 qt
    • Price
      41 USD
      750000000 USD

Nakajima C6N

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11
88.7
Height (m)
0.6
 
4.0
50.1
Wings
Wing area (m2)
1.1
 
22.5
925
Wingspan (Beam) (m)
0.1
 
12.5
95
Wing loading (kg/m2)
3.1
 
176
829
Weights
Empty weight (kg)
8
 
2,968
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,260
575,000
Loaded weight (kg)
5
 
4,500
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
610
28,165
at 6100 m
Сruise Speed (km/h)
52
 
387
3,087
Power
Total Power (hp)
0.4
 
1,990.6
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
10,470
161,544
Range (Ferry range) (km)
4
 
5,300
40,700
Сombat radius (km)
277
 
3,320
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
736
36,000
Time to altitude (min)
0.6
 
8.2
105
to 6000 m
Combat
Guns (qt)
1
 
1
18
flexibly mounted rearward-firing 7.92 mm Type 1 machine gun
Stat
Number built (qt)
0
 
463
43,000
Introduction 1944
First flight 15.05.1943
Stop production 1945

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