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    • Year
      1906
      2018
    • Length
      21 m
      33 m
    • Height
      6 m
      10 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
      17 m
      27 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
      3 m
      5 m
    • Empty weight
      8592 kg
      12888 kg
    • Max. takeoff weight (Gross weight)
      15240 kg
      22862 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
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      252 km/h
      378 km/h
    • Сruise Speed
      800 km/h
      1200 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
      1908 l
      2862 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
      6280 hp
      9420 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2852 m
      4278 m
    • Static ceiling
      3 m
      4 m
    • Range (Ferry range)
      800 km
      1200 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
      4084 m/min
      6127 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 CH-53 Sea Stallion

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
27.0
88.7
Height (m)
0.6
 
7.6
50.1
Rotors
Main rotor diameter (m)
1.2
 
22.0
62
Tail rotor diameter (m)
0.8
 
4.9
4.9
Weights
Empty weight (kg)
8
 
10,740
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
19,050.9
575,000
Capacity
Crew (per.)
1
 
3
112
2 pilots, 1 or more crew chiefs
Speeds
Max. Speed (km/h)
25
 
315
28,165
Сruise Speed (km/h)
52
 
1,000
3,087
Fuel
Fuel Capacity (l)
23
 
2,385
320,000
Power
Total Power (hp)
0.4
 
7,850
60,000
2 powerplants 3925 hp each
Performance
Service ceiling (m)
0.6
 
3,565
161,544
Static ceiling (m)
3
 
3
5,485
2 pilots, 1 or more crew chiefs
Range (Ferry range) (km)
4
 
1,000
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
5,105.4
36,000
Stat
Introduction 1964
First flight 14.10.1964
Stop production 2012

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