Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 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
      63 m2
      96 m2
    • Main rotor diameter
      8 m
      13 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
      2 m
      4 m
    • Empty weight
      598 kg
      899 kg
    • Max. takeoff weight (Gross weight)
      979 kg
      1470 kg
    • Loaded weight
      870 kg
      1307 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      3 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      141 km/h
      213 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      123 km/h
      186 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
      187 l
      282 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
      196 hp
      294 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      316 m/min
      476 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
      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
      74 qt
      112 qt
    • Price
      41 USD
      750000000 USD

Sikorsky S-52

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
8.4
88.7
fuselage length
Height (m)
0.6
 
2.6
50.1
Rotors
Disc area (m2)
1.4
 
79.4
460
Main rotor diameter (m)
1.2
 
10.1
62
Tail rotor diameter (m)
0.8
 
2.7
4.9
Weights
Empty weight (kg)
8
 
748.4
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,224.7
575,000
overload
Loaded weight (kg)
5
 
1,088.6
242,500
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
2
400
Speeds
Ground Speed (km/h)
96.6
 
177.0
1,500
at sea level
Сruise Speed (km/h)
52
 
154.5
3,087
Fuel
Fuel Capacity (l)
23
 
234.7
320,000
Power
Total Power (hp)
0.4
 
245
60,000
1 powerplant
Dynamic Performance
Rate of climb (m/min)
1.9
 
396.2
36,000
Stat
Number built (qt)
0
 
93
43,000
Introduction 1947
First flight 12.02.1947

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