Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      22 m2
      35 m2
    • Wingspan (Beam)
      8 m
      13 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
      800 kg
      1201 kg
    • Max. takeoff weight (Gross weight)
      1266 kg
      1900 kg
    • Loaded weight
      5 kg
      242500 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
      229 km/h
      345 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
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      352 hp
      528 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7144 m
      10717 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      352 km
      528 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
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      3 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
      354 qt
      532 qt
    • Price
      41 USD
      750000000 USD

Nakajima Bulldog Fighter

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.7
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
28.5
925
Wingspan (Beam) (m)
0.1
 
10.3
95
Weights
Empty weight (kg)
8
 
1,000.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,583.0
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
287
28,165
Power
Total Power (hp)
0.4
 
440
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,930.6
161,544
Range (Ferry range) (km)
4
 
440
40,700
Combat
Guns (qt)
1
 
2
18
0.303 in (7.7 mm) Vickers machine guns
Bombs (qt)
1
 
4
250
9 kg bombs
Stat
Number built (qt)
0
 
443
43,000
including prototypes and licence built
Introduction 1927
First flight 17.05.1927
Stop production 1937

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