Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      9 m
      15 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
      1529 kg
      2295 kg
    • Max. takeoff weight (Gross weight)
      2304 kg
      3456 kg
    • Loaded weight
      1968 kg
      2952 kg
    • Crew
      1 per.
      2 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
      348 km/h
      524 km/h
    • Сruise Speed
      240 km/h
      360 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
      760 hp
      1140 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8000 m
      12000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1425 km
      2139 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
      5 m/min
      9 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
      18 qt
    • Bombs
      3 qt
      5 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
      261 qt
      393 qt
    • Price
      41 USD
      750000000 USD

Nakajima A6M2-N

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
10.1
88.7
Height (m)
0.6
 
4.3
50.1
Wings
Wing area (m2)
1.1
 
22.4
925
Wingspan (Beam) (m)
0.1
 
12
95
Weights
Empty weight (kg)
8
 
1,912
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,880
575,000
Loaded weight (kg)
5
 
2,460
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
436
28,165
at 5000 m
Сruise Speed (km/h)
52
 
300
3,087
Power
Total Power (hp)
0.4
 
950
60,000
at 4200 m (1 powerplant)
Performance
Service ceiling (m)
0.6
 
10,000
161,544
Range (Ferry range) (km)
4
 
1,782
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
6.7
36,000
to 5000 m
Combat
Bombs (qt)
1
 
2
250
60 kg bombs
1
 
4
250
2 × 7.7 mm Type 97 machine guns in forward fuselage; 2 ×20 mm Type 99 cannons -fixed in outer wings
Stat
Number built (qt)
0
 
327
43,000
Introduction 1941
First flight 07.12.1941

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