Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      6 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
      183 m2
      275 m2
    • Main rotor diameter
      13 m
      21 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
      2866 kg
      4300 kg
    • Max. takeoff weight (Gross weight)
      5080 kg
      7621 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      12 per.
      20 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      222 km/h
      334 km/h
    • Сruise Speed
      126 km/h
      190 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
      1220 hp
      1830 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      1196 m
      1795 m
    • Static ceiling
      1584 m
      2376 m
    • Range (Ferry range)
      234 km
      352 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
      280 m/min
      420 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
      1686 qt
      2530 qt
    • Price
      41 USD
      750000000 USD

Sikorsky H-34

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
17.3
88.7
Height (m)
0.6
 
4.9
50.1
Rotors
Disc area (m2)
1.4
 
228.9
460
Main rotor diameter (m)
1.2
 
17.1
62
Tail rotor diameter (m)
0.8
 
2.9
4.9
Weights
Empty weight (kg)
8
 
3,583
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,350.3
575,000
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
16
400
16 troops or 8 stretchers
Speeds
Max. Speed (km/h)
25
 
278
28,165
Сruise Speed (km/h)
52
 
158
3,087
Power
Total Power (hp)
0.4
 
1,525
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
1,495.0
161,544
Static ceiling (m)
3
 
1,980
5,485
Range (Ferry range) (km)
4
 
293
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
350
36,000
Stat
Number built (qt)
0
 
2,108
43,000
Introduction 1970
First flight 08.03.1954

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