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    • 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
      29 m2
      45 m2
    • Wingspan (Beam)
      11 m
      18 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
      2408 kg
      3612 kg
    • Max. takeoff weight (Gross weight)
      4520 kg
      6780 kg
    • Loaded weight
      4160 kg
      6240 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
      384 km/h
      578 km/h
    • Сruise Speed
      264 km/h
      396 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
      1479 hp
      2220 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7232 m
      10848 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2436 km
      3656 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
      364 m/min
      546 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      8 min
      13 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
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      2 qt
    • Bombs weight
      640 kg
      960 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1014 qt
      1522 qt
    • Price
      41 USD
      750000000 USD

Nakajima B6N

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
10.9
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
37.3
925
Wingspan (Beam) (m)
0.1
 
14.9
95
Weights
Empty weight (kg)
8
 
3,010
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,650
575,000
Loaded weight (kg)
5
 
5,200
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
481
28,165
at 4900 m
Сruise Speed (km/h)
52
 
330
3,087
at 4000 m
Power
Total Power (hp)
0.4
 
1,849.9
60,000
1 powerplant (take-off power)
Performance
Service ceiling (m)
0.6
 
9,040
161,544
Range (Ferry range) (km)
4
 
3,046
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
455
36,000
Time to altitude (min)
0.6
 
10.4
105
to 5000 m
Combat
Guns (qt)
1
 
2
18
1 × 7.7 mm (0.303 in) Type 92 machine gun in rear cockpit and 1 × 7.7 mm (0.303 in) Type 92 firing through ventral tunnel
Torpedoes (qt)
1
 
1
4
800kg torpedo or
Bombs weight (kg)
2
 
800
39,000
of bombs
Stat
Number built (qt)
0
 
1,268
43,000
Introduction 1941
First flight 14.03.1941
Stop production 1945

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