Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      5 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
      134 m2
      202 m2
    • Main rotor diameter
      11 m
      18 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
      1371 kg
      2058 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1754 kg
      2632 kg
    • Crew
      1 per.
      3 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
      136 km/h
      206 km/h
    • Сruise Speed
      104 km/h
      156 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
      360 hp
      540 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3511 m
      5267 m
    • Static ceiling
      1696 m
      2544 m
    • Range (Ferry range)
      463 km
      696 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
      211 m/min
      317 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      12 min
      18 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
      240 qt
      360 qt
    • Price
      41 USD
      750000000 USD

Sikorsky H-5

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
17.4
88.7
Height (m)
0.6
 
4.0
50.1
Rotors
Disc area (m2)
1.4
 
168.2
460
Main rotor diameter (m)
1.2
 
14.6
62
Tail rotor diameter (m)
0.8
 
2.6
4.9
Weights
Empty weight (kg)
8
 
1,714.6
276,800
Loaded weight (kg)
5
 
2,193
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
171
28,165
Сruise Speed (km/h)
52
 
130
3,087
Power
Total Power (hp)
0.4
 
450
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,389.1
161,544
Static ceiling (m)
3
 
2,120
5,485
Range (Ferry range) (km)
4
 
579.7
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
264
36,000
Time to altitude (min)
0.6
 
15
105
to 3050 m
Stat
Number built (qt)
0
 
300
43,000
Introduction 1943
First flight 1943
Stop production 1957

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