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    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      4 m
      7 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
      224 m2
      337 m2
    • Main rotor diameter
      15 m
      23 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
      4476 kg
      6714 kg
    • Max. takeoff weight (Gross weight)
      6894 kg
      10342 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
      24 per.
      36 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      213 km/h
      321 km/h
    • Сruise Speed
      177 km/h
      267 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
      2544 l
      3816 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
      2400 hp
      3600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3048 m
      4572 m
    • Static ceiling
      1720 m
      2580 m
    • Range (Ferry range)
      666 km
      1000 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
      541 m/min
      812 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
      95 qt
      143 qt
    • Price
      41 USD
      750000000 USD

Sikorsky S-61

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Operation

Passenger

Cargo

Geometry
Length (m)
1.9
 
18.0
88.7
Height (m)
0.6
 
5.3
50.1
Rotors
Disc area (m2)
1.4
 
280.6
460
Main rotor diameter (m)
1.2
 
18.9
62
Tail rotor diameter (m)
0.8
 
3.2
4.9
Weights
Empty weight (kg)
8
 
5,595
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,618.3
575,000
Capacity
Crew (per.)
1
 
2
112
pilots
Capacity passengers (per.)
1
 
30
400
up to 30 passengers
Speeds
Max. Speed (km/h)
25
 
267
28,165
Сruise Speed (km/h)
52
 
222
3,087
Fuel
Fuel Capacity (l)
23
 
3,180
320,000
Power
Total Power (hp)
0.4
 
3,000
60,000
2 powerplants 1500 hp each
Performance
Service ceiling (m)
0.6
 
3,810
161,544
Static ceiling (m)
3
 
2,150
5,485
Range (Ferry range) (km)
4
 
833
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
676.7
36,000
400–670 m/min
Stat
Number built (qt)
0
 
119
43,000
Introduction 01.09.1961
First flight 11.03.1959

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