Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      40 m2
      60 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
      1109 kg
      1665 kg
    • Max. takeoff weight (Gross weight)
      2000 kg
      3000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      171 km/h
      257 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
      292 l
      438 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
      360 hp
      540 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5760 m
      8640 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      640 km
      960 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
      2 qt
      4 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
      2160 qt
      3240 qt
    • Price
      41 USD
      750000000 USD

Nakajima Nakajima-Breguet Reconnaissance Seaplane

TypeAircraft
Company

Nakajima Aircraft Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.6
88.7
Height (m)
0.6
 
3.7
50.1
Wings
Wing area (m2)
1.1
 
50
925
Wingspan (Beam) (m)
0.1
 
14.8
95
Weights
Empty weight (kg)
8
 
1,387
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,500
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
214
28,165
Fuel
Fuel Capacity (l)
23
 
365
320,000
Power
Total Power (hp)
0.4
 
450
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,200
161,544
Range (Ferry range) (km)
4
 
800
40,700
Combat
Guns (qt)
1
 
3
18
1 x fixed, forward-firing 7.7 mm (0.30 in) Vickers machine gun; 2 x flexible, rearward-firing 7.7 mm (0.30 in) Lewis Guns
Stat
Number built (qt)
0
 
2,700
43,000
Introduction 1925
First flight 01.03.1922

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