Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      2 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
      1 m2
      460 m2
    • Main rotor diameter
      9 m
      14 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
      1 m
    • Empty weight
      628 kg
      944 kg
    • Max. takeoff weight (Gross weight)
      1081 kg
      1623 kg
    • Loaded weight
      943 kg
      1416 kg
    • Crew
      1 per.
      2 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
      128 km/h
      194 km/h
    • Сruise Speed
      88 km/h
      134 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
      192 hp
      288 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2438 m
      3658 m
    • Static ceiling
      1760 m
      2640 m
    • Range (Ferry range)
      392 km
      590 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
      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
      180 qt
      270 qt
    • Price
      41 USD
      750000000 USD

Sikorsky R-6 Hoverfly II

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
14.6
88.7
Height (m)
0.6
 
3.5
50.1
Rotors
Main rotor diameter (m)
1.2
 
11.6
62
Tail rotor diameter (m)
0.8
 
0.8
4.9
Weights
Empty weight (kg)
8
 
786
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,352
575,000
Loaded weight (kg)
5
 
1,179.3
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
160.9
28,165
Сruise Speed (km/h)
52
 
111
3,087
Power
Total Power (hp)
0.4
 
240
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,048
161,544
Static ceiling (m)
3
 
2,200
5,485
Range (Ferry range) (km)
4
 
491
40,700
Stat
Number built (qt)
0
 
225
43,000
Introduction 1943
First flight 15.10.1943

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