External Lift

The Sikorsky CH-53K King Stallion completed an external lift of a 36,000-pound/16,330-kg payload at the Sikorsky Development Flight Center, achieving a maximum weight on the single center point cargo hook. This milestone marks completion of critical flight envelope expansion activities for the CH-53K King Stallion as Sikorsky, a Lockheed Martin company prepares to deliver the first aircraft to the U.S. Marine Corps this year.

The Sikorsky CH-53K King Stallion helicopter achieves a 36,000-pound/16,330-kg lift for the first time at Sikorsky Development Flight Center in West Palm Beach, Florida, on February 10, 2018 (Image courtesy Sikorsky, a Lockheed Martin Company)
The Sikorsky CH-53K King Stallion helicopter achieves a 36,000-pound/16,330-kg lift for the first time at Sikorsky Development Flight Center in West Palm Beach, Florida, on February 10, 2018 (Image courtesy Sikorsky, a Lockheed Martin Company)

The CH-53K King Stallion lifted the external load of 36,000 lbs./16,330 kg into a hover followed by flight demonstrating satisfactory handling qualities and structural margins. The gross weight of the aircraft topped out at just over 91,000 lbs./41,277 kg, making this the heaviest helicopter ever flown by Sikorsky.

«The successful completion of these last critical envelope expansion tests further demonstrates the maturity of the CH-53K aircraft», said Doctor Michael Torok, Sikorsky Vice President, Marine Corps Systems. «We look forward to bringing this unique and exceptional heavy lift capability to the United States Marine Corps and our international customers».

Prior to the 36,000-lb./16,330 kg lift, the CH-53K King Stallion lifted various external payloads up to 27,000 lbs./12,247 kg including a Joint Light Tactical Vehicle (JLTV). The CH-53K can carry a 27,000 lb./12,247 kg external load over 110 nautical miles/126.6 miles/203.7 km in high/hot conditions, which is more than triple the external load carrying capacity of the legacy CH-53E Super Stallion aircraft. Other flight envelope accomplishments include tethered hover demonstrating flight speeds to 200 knots/230 mph/370 km/h, angle of bank to 60 degrees, takeoffs and landings from sloped surfaces up to 12 degrees, external load auto-jettison, and gunfire testing.

«The payload capability of this helicopter is unmatched, triple that of its predecessor and better than any other heavy lift helicopter in production», said Colonel Hank Vanderborght, U.S. Marine Corps Program Manager for the Naval Air Systems Command’s Heavy Lift Helicopters Program. «The CH-53K program continues on pace to deploy this incredible heavy lift capability to our warfighters».

The CH-53K King Stallion is also garnering international interest. Rheinmetall and Sikorsky recently signed a strategic teaming agreement to offer the CH-53K King Stallion for Germany’s new heavy lift helicopter competition. Additional teammates will be announced in the coming weeks leading up to the aircraft’s debut at the ILA Berlin Air Show in April.

 

General Characteristics

Number of Engines 3
Engine Type T408-GE-400
T408 Engine 7,500 shp/5,595 kw
Maximum Gross Weight (Internal Load) 74,000 lbs/33,566 kg
Maximum Gross Weight (External Load) 88,000 lbs/39,916 kg
Cruise Speed 141 knots/162 mph/261 km/h
Range 460 NM/530 miles/852 km
AEO* Service Ceiling 14,380 feet/4,383 m
HIGE** Ceiling (MAGW) 13,630 feet/4,155 m
HOGE*** Ceiling (MAGW) 10,080 feet/3,073 m
Cabin Length 30 feet/9.1 m
Cabin Width 9 feet/2.7 m
Cabin Height 6.5 feet/2.0 m
Cabin Area 264.47 feet2/24.57 m2
Cabin Volume 1,735.36 feet3/49.14 m3

* All Engines Operating

** Hover Ceiling In Ground Effect

*** Hover Ceiling Out of Ground Effect

The Sikorsky CH-53K King Stallion completed an external lift of a 36,000-pound/16,330-kg payload at the Sikorsky Development Flight Center, achieving a maximum weight on the single center point cargo hook

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