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    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      7 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      77 m2
      117 m2
    • Wingspan (Beam)
      26 m
      41 m
    • Wing loading
      240 kg/m2
      360 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
      9973 kg
      14961 kg
    • Max. takeoff weight (Gross weight)
      23586 kg
      35381 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      8 per.
      14 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
      385 km/h
      579 km/h
    • Сruise Speed
      180 km/h
      270 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
      4320 hp
      6480 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5120 m
      7681 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3632 km
      5448 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
      9 qt
      15 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      4640 kg
      6960 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      591 qt
      887 qt
    • Price
      41 USD
      750000000 USD

Consolidated PB4Y-2 Privateer

TypeAircraft
Company

Consolidated Aircraft Corporation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
22.7
88.7
Height (m)
0.6
 
9.2
50.1
Wings
Wing area (m2)
1.1
 
97.4
925
Wingspan (Beam) (m)
0.1
 
33.5
95
Wing loading (kg/m2)
3.1
 
300
829
Weights
Empty weight (kg)
8
 
12,467.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
29,483.5
575,000
Capacity
Crew (per.)
1
 
11
112
two pilots, navigator, bombardier, five gunners, two radio operators
Speeds
Max. Speed (km/h)
25
 
482
28,165
Сruise Speed (km/h)
52
 
225
3,087
Power
Total Power (hp)
0.4
 
5,400
60,000
4 powerplants 1350 hp each
Performance
Service ceiling (m)
0.6
 
6,400.8
161,544
Range (Ferry range) (km)
4
 
4,540
40,700
Combat
Guns (qt)
1
 
12
18
.50 in (12.7 mm) M2 Browning machine guns in six turrets
Bombs weight (kg)
2
 
5,800
39,000
of bombs, mines, or torpedoes
Stat
Number built (qt)
0
 
739
43,000
Introduction 1943
Stop production 1954

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