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    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      104 m2
      157 m2
    • Wingspan (Beam)
      25 m
      39 m
    • Wing loading
      98 kg/m2
      149 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      6
      10
    • 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
      7587 kg
      11382 kg
    • Max. takeoff weight (Gross weight)
      12852 kg
      19280 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      8 per.
      12 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
      251 km/h
      377 km/h
    • Сruise Speed
      160 km/h
      242 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
      1920 hp
      2880 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3224 km
      4836 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
      243 m/min
      366 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
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1451 kg
      2177 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      245 qt
      369 qt
    • Price
      72000 USD
      108000 USD

Boeing Boeing-Canada PB2B-1

TypeAircraft
Company

Boeing

Scheme

Parasol

Monoplane

Geometry
Length (m)
1.9
 
19.5
88.7
Height (m)
0.6
 
6.2
50.1
Wings
Wing area (m2)
1.1
 
130.1
925
Wingspan (Beam) (m)
0.1
 
31.7
95
Wing loading (kg/m2)
3.1
 
123.6
829
Aspect ratio
1.7
 
7.7
25.6
Weights
Empty weight (kg)
8
 
9,484.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
16,066.2
575,000
Capacity
Crew (per.)
1
 
10
112
pilot, co-pilot, bow turret gunner, flight engineer, radio operator, navigator, radar operator, two waist gunners, ventral gunner
Speeds
Max. Speed (km/h)
25
 
314
28,165
Сruise Speed (km/h)
52
 
201
3,087
Power
Total Power (hp)
0.4
 
2,400
60,000
2 powerplants 1200 hp each
Performance
Service ceiling (m)
0.6
 
4,000
161,544
Range (Ferry range) (km)
4
 
4,030
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
304.8
36,000
Combat
Guns (qt)
1
 
6
18
3 x .30 cal (7.62 mm) machine guns (two in nose turret, one in ventral hatch at tail); 2 x .50 cal (12.7 mm) machine guns (one in each waist blister)
Bombs weight (kg)
2
 
1,814
39,000
of bombs or depth charges; torpedo racks were also available
Stat
Number built (qt)
0
 
307
43,000
by Boeing Canada
Price (USD)
41.5
 
90,000
750.0 million
Introduction 1935
First flight 28.03.1935
Stop production 1957

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