Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      30 m2
      46 m2
    • Wingspan (Beam)
      12 m
      19 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
      1823 kg
      2735 kg
    • Max. takeoff weight (Gross weight)
      3280 kg
      4920 kg
    • Loaded weight
      5 kg
      242500 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
      302 km/h
      454 km/h
    • Сruise Speed
      204 km/h
      306 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
      800 hp
      1200 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6608 m
      9912 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1593 km
      2391 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
      312 m/min
      468 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
      1 qt
      2 qt
    • Bombs
      1 qt
      2 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      2 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      919 qt
      1379 qt
    • Price
      41 USD
      750000000 USD

Nakajima B5N

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
10.3
88.7
Height (m)
0.6
 
3.7
50.1
Wings
Wing area (m2)
1.1
 
37.7
925
Wingspan (Beam) (m)
0.1
 
15.5
95
Weights
Empty weight (kg)
8
 
2,279
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,100
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
378
28,165
Сruise Speed (km/h)
52
 
255
3,087
Power
Total Power (hp)
0.4
 
1,000
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,260
161,544
Range (Ferry range) (km)
4
 
1,992
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
390
36,000
Combat
Guns (qt)
1
 
1
18
7.7 mm Type 92 machine gun 'Ru' (Lewis) in rear dorsal position
Bombs (qt)
1
 
6
250
132 kg (293 lb) bombs or
1
 
2
250
250 kg (550 lb) bombs or
1
 
1
250
800kg (1,760lb) bomb or
1
 
1
250
Torpedoes (qt)
1
 
1
4
800 kg (1,760 lb) type 91 torpedo
Stat
Number built (qt)
0
 
1,149
43,000
Introduction 1937
First flight 1937
Stop production 1945

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