WebThe first CH-53As were powered by two General Electric T64-GE-6 turboshaft engines with 2,850 shp (2,125 kW) and had a maximum gross weight of 46,000 lb (20,865 kg) including 20,000 lb (9,072 kg) in payload. Variants of the original CH-53A Sea Stallion include the RH-53A/D, HH-53B/C, CH-53D, CH-53G, and MH-53H/J/M. WebDec 27, 2024 · The CH-53K is the Marine Corps' new build, heavy lift replacement for the CH-53E. The US plans to buy 200 King Stallions. The fly-by-wire, triple-engine aircraft is designed with roughly three ...
Sikorsky MH-53 - Wikipedia
WebSpecifications (CH-53D) Data from Deagel.com, U.S. Navy history, International Directory, US Navy Fact File. General characteristics. Crew: 2 pilots, 1 or more crew chiefs Capacity: 38 troops (55 in alternate configuration) or 24 stretchers Length: 88 ft 6 in (26.97 m) Rotor diameter: 72 ft 2.8 in (22.01 m) Height: 24 ft 11 in (7.6 m) Disc area: 4098.1 sq ft (380.48 … WebAnother heavy lift helicopter, the Sikorsky CH-53 Sea Stallion, had also been developed using many of the proven systems of the CH-54, including its engine, fuselage, and dynamic systems. ... Empty weight: 19,800 lb … saints community songs
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The Sikorsky CH-53 Sea Stallion is a heavy lift military transport helicopter. The CH-53A carries a crew of four; pilot, copilot, crew chief, and an aerial observer. It can carry various payloads, including up to 38 fully-equipped troops, 24 litters with medical attendants, an internal cargo load of 8,000 pounds (3,600 kg), or … See more The CH-53 Sea Stallion (Sikorsky S-65) is an American family of heavy-lift transport helicopters designed and built by the American manufacturer Sikorsky Aircraft. It was originally developed in response to a request from the See more United States The CH-53/HH-53 has seen considerable use in warzones and served in various conflict during its service. It was first used in the Vietnam War, often recovering downed aircraft and evacuating personnel. The CH-53D … See more Israel On display • Israeli Air Force Museum United States See more Data from Deagel.com, U.S. Navy history, International Directory, US Navy Fact File General characteristics • Crew: 2 pilots, 1 or more loadmasters / crewmen • Capacity: 38 troops (55 in alternate configuration) or 24 stretchers / 8,000 lb (3,600 kg) … See more Origins In 1960, the United States Marine Corps (USMC) began to seek a replacement for their See more For other variants, see HH-53 "Super Jolly Green Giant"/MH-53 Pave Low and CH-53E Super Stallion. YCH-53A Two prototypes with two 2,850 shp (2,130 kW) T64-GE-3 engines. CH-53A Initial production variant for the USMC. 139 built. … See more Due to the aircraft's large size and troop capacity, aerial accidents involving CH-53 helicopters have been some of the deadliest helicopter accidents. • 23 … See more WebLoaded weight: 33,500 lb (15,227 kg) Useful load: 8,000 lb (3,630 kg) Max. takeoff weight: 42,000 lb (19,100 kg) Powerplant: 2 × General Electric T64-GE-413 turboshaft, 3,925 … http://www.aviatorsdatabase.com/wp-content/uploads/2013/07/CH-53K-Helicopter.pdf saints community church fresno ca