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Sikorsky CH-53K/S-95
King Stallion

General information
Type Heavy transport helicopter
National origin United States
Manufacturer Sikorsky Aircraft
Status In production
Primary user United States Marine Corps
Number built 19 (circa early 2023)
History
Introduction date May 2018 (Delivered to USMC)22 April 2022 (IOC)
First flight 27 October 2015
Developed from Sikorsky CH-53E Super Stallion
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History Sikorsky 
Sikorsky CH-53K King Stallion
date May 2018 (Delivered to USMC) 22 April 2022 (IOC)
First flight 27 October 2015

The United States Marine Corps plans to receive 200 helicopters at a total cost of $25 billion. Ground Test Vehicle (GTV) testing started in April 2014; flight testing began with the maiden flight on 27 October 2015. In May 2018, the first CH-53K was delivered to the Marine Corps. On 22 April 2022, it was declared to have passed initial operational capability. Israel has also reportedly ordered the type; other potential export customers include Japan and Germany

The CH-53K King Stallion is a heavy lift helicopter, being a general redesign of the preceding CH-53E, the main improvements being the new engines and cockpit layout. It has over twice the lift capacity and radius of action of the CH-53E, and a wider cargo hold to allow it to carry a Humvee internally. A new composite rotor blade system is also used, featuring technology similar to that of the UH-60 Black Hawk helicopter. The CH-53K is powered by the General Electric GE38-1B engine, which was selected over the Pratt and Whitney Canada PW150 and a variant of the Rolls-Royce AE 1107C-Liberty used on the V-22 Osprey. Each of the three T408 engines is rated at 7,500 shp (5,600 kW), and gives the CH-53K the ability to fly 20 knots (37 km/h; 23 mph) faster than its CH-53E predecesso

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Howard Sikorsky helicopters MD

Sikorsky, a Lockheed Martin Company
Sikorsky CH-53K King Stallion

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General Info

  • Crew: 4
  • Capacity: 30 passengers or troops / 24x casualty litters 35,000 lb (15,876 kg) payload
    • Centre external load hook rating – 36,000 lb (16,329 kg)
    • Fore and aft external load hooks rating – 25,200 lb (11,431 kg)
    • Internal cargo system:
    • Length: 99 ft (30 m) rotor and tail un-folded Width: 17 ft 6 in (5.33 m) fuselage Height: 28 ft 4.9 in (8.659 m) rotor and tail un-folded
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Powerplant

  • Max takeoff weight: 88,000 lb (39,916 kg) with external load
  • 74,000 lb (33,566 kg) with maximum internal load
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Specifications

  • Cruise speed: 170 kn (200 mph, 310 km/h)
  • Range: 460 nmi (530 mi, 850 km)
  • Combat range: 110 nmi (130 mi, 200 km)
  • Service ceiling: 16,000 ft (4,900 m) ISA
  • 13,200 ft (4,023 m) ISA +24 °C (75 °F)
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Armament

Special Links Sikorsky CH-53K King Stallion

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The UH-60 entered service with the U.S. Army's 101st Combat Aviation Brigade of the 101st Airborne Division in June 1979.[92] The U.S. military first used the UH-60 in combat during the invasion of Grenada in 1983.

Sikorsky CH-53K
King Stallion

The Sikorsky CH-53K King Stallion (Sikorsky S-95) is a heavy-lift cargo helicopter

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Youtube Link

he Sikorsky CH-53K King Stallion (Sikorsky S-95) is a heavy-lift cargo helicopter

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