Sikorsky CH-53E Super Stallion
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From Wikipedia
The Sikorsky CH-53E Super Stallion is a heavy lift helicopter operated by the United States military. As the Sikorsky S-80, it was developed from the CH-53 Sea Stallion, mainly by adding a third engine, adding a seventh blade to the main rotor, and canting the tail rotor 20°. It was built by Sikorsky Aircraft for the United States Marine Corps. Developed in the 1970s, it entered service in 1981, and is planned to be in service into the 2030s. It is one of the largest military helicopters in service, and is operated from U.S. Navy ships or from land.
Summary of “Sikorsky CH-53E Super Stallion” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the Sikorsky CH-53E Super Stallion by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/H53/), CC BY 4.0Specifications
- Length
- 30.2 m99.1 ft
- Rotor diameter
- 24.08 m79 ft
- Max take-off weight
- 33.3 t73,400 lb
- Cruise speed
- 278 km/h173 mph
- Max speed
- 315 km/h196 mph
- Range
- 1,000 km621 mi
- Ceiling
- 5,639 m18,500 ft
- Engines
- 3× GE T64 (turboshaft)
- Power
- 3× 4 380 hp
- First flight
- 1974
- In service
- 1981
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.
