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    • Year
      1906
      2018
    • Length
      53 m
      81 m
    • Height
      4 m
      7 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
      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
      29200 kg
      43800 kg
    • Max. takeoff weight (Gross weight)
      23586 kg
      35381 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
      232 km/h
      348 km/h
    • Сruise Speed
      276 km/h
      416 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
      965 hp
      1448 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6827 m
      10242 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1680 km
      2520 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
      249 m/min
      375 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
      8 qt
      12 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
      15404 qt
      23108 qt
    • Price
      238101 USD
      357153 USD

Consolidated P5Y

TypeAircraft
Company

Consolidated Aircraft Corporation

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
67
88.7
Height (m)
0.6
 
5.5
50.1
Wings
Wing area (m2)
1.1
 
97.5
925
Wingspan (Beam) (m)
0.1
 
33.5
95
Weights
Empty weight (kg)
8
 
36,500
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
29,483.5
575,000
Capacity
Crew (per.)
1
 
10
112
Speeds
Max. Speed (km/h)
25
 
290
28,165
Сruise Speed (km/h)
52
 
346
3,087
Power
Total Power (hp)
0.4
 
1,206.4
60,000
Performance
Service ceiling (m)
0.6
 
8,534.4
161,544
Range (Ferry range) (km)
4
 
2,100
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
312.4
36,000
Combat
Guns (qt)
1
 
10
18
Stat
Number built (qt)
0
 
19,256
43,000
Price (USD)
41.5
 
297,627
750.0 million
Introduction 1943
First flight 29.12.1939
Stop production 1968

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