Vehicle

Sikorsky CH-53E Super Stallion

Lighter-Than-Air Craft and Rotorcraft

The Sikorsky CH-53E Super Stallion, company model S-80, is a heavy-lift helicopter built by Sikorsky Aircraft for the US Marine Corps. It developed from the CH-53 Sea Stallion by adding a third engine, a seventh main rotor blade and a tail rotor canted 20 degrees. The YCH-53E first flew in 1974, the type entered service in 1981 and it is planned to serve into the 2030s. It is one of the largest military helicopters in service and operates from Navy ships or from land. The Navy flies the related MH-53E Sea Dragon for mine countermeasures and heavy lift, and the CH-53K King Stallion is set to replace the CH-53E.

Facts
Year
1974 1
Engine Class
Turboshaft 1
Status
In service 1
Units Built
170 1
Top Speed (km/h)
310 1
Mass (kg)
15,071 1
Maximum Mass (kg)
33,339 1
Comparison
Body Style
Helicopter 1
Sikorsky CH-53E Super Stallion
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Exemplifies

Source Sikorsky CH-53E Super Stallion (Wikipedia)

Of Make

Source Sikorsky CH-53E Super Stallion (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Sikorsky CH-53E Super Stallion (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
It was built by Sikorsky Aircraft for the United States Marine Corps.

Originated In

Also in Geography Atlas: where this subject originated.

Source Sikorsky CH-53E Super Stallion (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
It was built by Sikorsky Aircraft for the United States Marine Corps.
Sources
1. Sikorsky CH-53E Super Stallion (Wikipedia)
  • Development
    In 1974, the initial YCH-53E first flew.
  • Specifications (CH-53E)
    Powerplant: 3 × General Electric T64-GE-416 / GE-416A / GE-419 turboshaft engines
  • Lead
    Developed in the 1970s, it entered service in 1981, and is planned to be in service into the 2030s.
  • Variants
    United States military designation for the S-80E heavy lift transport variant for the United States Navy and Marine Corps, 170 built.
  • Specifications (CH-53E), mass
    Empty weight: 33,226 lb (15,071 kg)
  • Specifications (CH-53E), maximum mass
    Max takeoff weight: 73,500 lb (33,339 kg)
  • Specifications (CH-53E), top speed
    Maximum speed: 170 kn (200 mph, 310 km/h)
  • Lead, manufacturer
    It was built by Sikorsky Aircraft for the United States Marine Corps.
  • Lead sentence
    The Sikorsky CH-53E Super Stallion is a heavy lift helicopter operated by the United States military.
  • Has Part: General Electric T64, Design, H-53 variants
    a more powerful version of the General Electric T64 engine, used in all H-53 variants
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