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    • Year
      1906
      2018
    • Length
      12 m
      20 m
    • Height
      3 m
      6 m
    • Width
      2 m
      4 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
      10 m
      17 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
      1 m
      3 m
    • Empty weight
      2541 kg
      3813 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      4245 kg
      6369 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
      229 km/h
      345 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      229 km/h
      345 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
      851 l
      1277 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
      1475 hp
      2213 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3360 m
      5040 m
    • Static ceiling
      1325 m
      1989 m
    • Range (Ferry range)
      462 km
      694 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
      365 m/min
      549 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
      872 qt
      1308 qt
    • Price
      10400000 USD
      15600000 USD

Sikorsky S-76

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
16
88.7
from tip of main rotor to tip of tail rotor
Height (m)
0.6
 
4.4
50.1
to tip of tail rotor
Width (m)
1.9
 
3.1
7.7
at horizontal stabilizer
Rotors
Main rotor diameter (m)
1.2
 
13.4
62
Tail rotor diameter (m)
0.8
 
2.4
4.9
Weights
Empty weight (kg)
8
 
3,177
276,800
in utility configuration
Loaded weight (kg)
5
 
5,307
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
287
1,500
at maximum takeoff weight at sea level in standard atmospheric conditions
Сruise Speed (km/h)
52
 
287
3,087
maximum cruise speed is the same as maximum speed
Fuel
Fuel Capacity (l)
23
 
1,064
320,000
Power
Total Power (hp)
0.4
 
1,844
60,000
2 powerplants 922 hp each
Performance
Service ceiling (m)
0.6
 
4,200
161,544
Static ceiling (m)
3
 
1,657
5,485
Range (Ferry range) (km)
4
 
578
40,700
no reserves, at long-range cruise speed at 1 220 m altitude
Dynamic Performance
Rate of climb (m/min)
1.9
 
457
36,000
Stat
Number built (qt)
0
 
1,090
43,000
Price (USD)
41.5
 
13.0 million
750.0 million
Introduction 1977
First flight 13.03.1977

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