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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      29 m2
    • Wingspan (Beam)
      6 m
      11 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
      1024 kg
      1538 kg
    • Max. takeoff weight (Gross weight)
      1344 kg
      2016 kg
    • Loaded weight
      1344 kg
      2016 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
      257 km/h
      387 km/h
    • Сruise Speed
      219 km/h
      329 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
      500 hp
      750 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5280 m
      7920 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      676 km
      1014 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
      289 m/min
      435 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
      1 qt
      3 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      181 kg
      273 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Boeing XF6B-1

TypeAircraft
Company

Boeing

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.7
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
23.4
925
Wingspan (Beam) (m)
0.1
 
8.7
95
Weights
Empty weight (kg)
8
 
1,281
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,680
575,000
Loaded weight (kg)
5
 
1,680
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
322
28,165
Сruise Speed (km/h)
52
 
274
3,087
Power
Total Power (hp)
0.4
 
625
60,000
Performance
Service ceiling (m)
0.6
 
6,600
161,544
Range (Ferry range) (km)
4
 
845
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
362.4
36,000
Combat
Bombs (qt)
1
 
2
250
.30in machine guns
Bombs weight (kg)
2
 
227
39,000
Stat
Number built (qt)
0
 
1
43,000
Introduction 1933
First flight 01.02.1933

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