Search filter

    • Year
      1906
      2018
    • Length
      24 m
      37 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      63 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
      368 m2
      460 m2
    • Main rotor diameter
      19 m
      29 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
      12056 kg
      18086 kg
    • Max. takeoff weight (Gross weight)
      26671 kg
      40007 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      10880 kg
      16320 kg
    • Payload
      10880 kg
      16320 kg
    • Capacity passengers
      29 per.
      45 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      136 km/h
      204 km/h
    • Сruise Speed
      222 km/h
      334 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
      3506 hp
      5261 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4511 m
      6767 m
    • Static ceiling
      2852 m
      4278 m
    • Range (Ferry range)
      800 km
      1201 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
      609 m/min
      915 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
      187 qt
      281 qt
    • Price
      19488000 USD
      29232000 USD

Sikorsky CH-53E Super Stallion

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
30.2
88.7
Height (m)
0.6
 
8.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
79
95
Rotors
Disc area (m2)
1.4
 
460
460
Main rotor diameter (m)
1.2
 
24.1
62
Tail rotor diameter (m)
0.8
 
4.9
4.9
Weights
Empty weight (kg)
8
 
15,071.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
33,339.0
575,000
Capacity
Crew (per.)
1
 
2
112
Useful load (kg)
26.4
 
13,600
90,700
Payload (kg)
23
 
13,600
122,470
Capacity passengers (per.)
1
 
37
400
Speeds
Max. Speed (km/h)
25
 
170
28,165
Сruise Speed (km/h)
52
 
278
3,087
Fuel
Fuel Capacity (l)
23
 
2,385
320,000
Fuel External (l)
142.5
 
-1
10,025
Power
Total Power (hp)
0.4
 
4,383.4
60,000
Performance
Service ceiling (m)
0.6
 
5,638.8
161,544
Static ceiling (m)
3
 
3,565
5,485
Range (Ferry range) (km)
4
 
1,000.1
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
762
36,000
Stat
Number built (qt)
0
 
234
43,000
Price (USD)
41.5
 
24.4 million
750.0 million
Introduction 1974
First flight 01.03.1974

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