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    • Year
      1906
      2018
    • Length
      17 m
      27 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
      1 m2
      460 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
      4840 kg
      7262 kg
    • Max. takeoff weight (Gross weight)
      8001 kg
      12003 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      212 km/h
      318 km/h
    • Сruise Speed
      198 km/h
      298 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
      2068 l
      3102 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
      4267 m
      6401 m
    • Static ceiling
      2960 m
      4440 m
    • Range (Ferry range)
      1003 km
      1505 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
      320 m/min
      480 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Sikorsky S-61R

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
22.3
88.7
Height (m)
0.6
 
5.5
50.1
Rotors
Main rotor diameter (m)
1.2
 
18.9
62
Blades per rotor (qt)
4
 
5
5
Tail rotor diameter (m)
0.8
 
3.2
4.9
Weights
Empty weight (kg)
8
 
6,051
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
10,001.7
575,000
Capacity
Crew (per.)
1
 
3
112
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
265
28,165
Сruise Speed (km/h)
52
 
248
3,087
Fuel
Fuel Capacity (l)
23
 
2,585
320,000
Power
Total Power (hp)
0.4
 
3,000
60,000
2 powerplants 1500 hp each
Performance
Service ceiling (m)
0.6
 
5,334
161,544
Static ceiling (m)
3
 
3,700
5,485
Range (Ferry range) (km)
4
 
1,254
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
400
36,000
400-670 m/min
Stat
Introduction 1961
First flight 1959

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