Community hub
Recent from talks
Knowledge base stats:
Talk channels stats:
Members stats:
Sikorsky CH-53 Sea Stallion
The CH-53 Sea Stallion (Sikorsky S-65) is a family of American heavy-lift transport helicopters designed and built by the American manufacturer Sikorsky Aircraft. The Sea Stallion was originally developed in response to a request from the United States Navy's Bureau of Naval Weapons made in March 1962 for a replacement for the Sikorsky CH-37 Mojave helicopters flown by the United States Marine Corps (USMC).
In July 1962, Sikorsky's proposal, which was essentially a scaled-up S-61R fitted with twin General Electric T64 turboshaft engines and the dynamic systems of the S-64/CH-54, was selected. On 14 October 1964, the YCH-53A performed its maiden flight; the first deliveries of production CH-53s to operational units commenced on 12 September 1966. The first combat use of the type occurred during the following year when it was deployed to the Vietnamese theater; the CH-53 quickly proved its value for moving heavy payloads, particularly in the recovery of damaged aircraft.
Several variants of the type were promptly introduced. The United States Air Force introduced the HH-53 "Super Jolly Green Giant", configured for special operations and combat search and rescue (CSAR) missions, during the latter part of the Vietnam War; the majority of these were subsequently rebuilt into the MH-53 Pave Low. The visually similar CH-53E Super Stallion is a heavier-lifting improved version of the rotorcraft, designated S-80E by Sikorsky; its third engine makes it more powerful than the Sea Stallion and thus displaced it for the heavy-lift mission. Furthermore, many early-build CH-53s were refitted with more powerful engines, while others were reconfigured for different mission roles, such as US presidential flights, training, and airborne mine countermeasures (AMCM) operations.
Several export deals for the CH-53 were made, leading to several international operators of the type. Among these are Germany, Iran, and Israel. Several unusual or high-profile operations have been undertaken, such as the capture and transportation of a Soviet advanced radar system to Israel under Operation Rooster 53 in 1969, and Iran's capture of five American CH-53s as a result of Operation Eagle Claw in 1980. Various operators deployed their CH-53s during international missions, often under the auspices of NATO or the United Nations, such as for UNSCOM in Iraq, in Kosovo with Kosovo Force (KFOR), Implementation Force (IFOR) in Bosnia and Herzegovina, and the International Security Assistance Force (ISAF) in Afghanistan. While several operators have opted to retain the type into the twenty-first century, many others have opted to supplement or withdraw their Sea Stallions in favor of other platforms, sometimes with the more powerful CH-53E. The CH-53 remains in service with German and Israeli forces, and is one of the largest military helicopters in service. Germany is planning to replace its fleet, as of the 2020s, with the latest version of the twin-rotor CH-47 Chinook. The latest version of the CH-53, the K model King Stallion is in production as of the 2020s entering service with the United States Marine Corps; this is replacing the Super Stallion, itself an upgraded version of Sea Stallion. The heavily upgraded Jolly Green Giant and Pave Low versions of the CH-53 were retired by 2008, flown by the U.S. Air Force for combat search and rescue. Overall, the CH-53 was replaced in many roles by the V-22 Osprey tilt rotor in U.S. service.
In 1960, the United States Marine Corps (USMC) began to seek a replacement for their HR2S piston-powered helicopters. On 27 January 1961, the USMC began working with the U.S. Army, Navy, and Air Force on the "Tri-Service VTOL transport", which would eventually emerge as the LTV XC-142 tiltwing. The design became more elaborate and the program stretched out, causing the USMC to drop out when they decided they would not receive a working machine in a satisfactory timeframe. In particular, there were concerns that the high levels of downwash produced by the XC-142A would render shipborne operations impractical. In the end, the XC-142A, although a very innovative and capable machine, never entered production.
In March 1962, the United States Navy's Bureau of Naval Weapons, acting on behalf of the USMC, issued a request for a "Heavy Helicopter Experimental / HH(X)". The specifications dictated a load capability of 8,000 pounds (3,600 kg) with an operational radius of 100 nautical miles (190 km; 120 mi) at a speed of 150 knots (280 km/h; 170 mph). It was also specified to possess a higher top speed and greater lifting capacity than existing helicopters while also having a lower empty weight than preceding designs as well. The HH(X) was to be used in the assault transport, aircraft recovery, personnel transport, and medical evacuation roles. In the assault transport role, it was to be mostly used to haul heavy equipment instead of troops.
In response, Boeing Vertol offered a modified version of the CH-47 Chinook; Kaman Aircraft offered a development of the British Fairey Rotodyne compound helicopter; and Sikorsky offered what amounted to a scaled-up version of the S-61R, with twin General Electric T64 turboshaft engines and the dynamic system of the S-64/CH-54, to be designated the S-65. Kaman's proposal quickly died when the British government dropped its backing of the Rotodyne program. Competition between Boeing Vertol and Sikorsky was intense, with the Chinook having an advantage because it was being acquired by the United States Army. During July 1962, it was announced that Sikorsky's bid had been selected as the winner on account of various considerations, including cost, technical factors, and production capability. However, a contract was not immediately forthcoming due to budgetary limitations.
The USMC had originally sought to procure four prototypes. However, in light of funding shortfalls, Sikorsky, determined to keep the deal, reduced their estimate for the program's development costs by proposing that development could be performed with only two prototypes. Military officials favorably received the company's proposed reduction; in September 1962, Sikorsky was awarded a $9,965,635 (~$78.9 million in 2024) contract for the production of a pair of YCH-53A prototypes, as well as a mockup and a ground-test airframe.
Hub AI
Sikorsky CH-53 Sea Stallion AI simulator
(@Sikorsky CH-53 Sea Stallion_simulator)
Sikorsky CH-53 Sea Stallion
The CH-53 Sea Stallion (Sikorsky S-65) is a family of American heavy-lift transport helicopters designed and built by the American manufacturer Sikorsky Aircraft. The Sea Stallion was originally developed in response to a request from the United States Navy's Bureau of Naval Weapons made in March 1962 for a replacement for the Sikorsky CH-37 Mojave helicopters flown by the United States Marine Corps (USMC).
In July 1962, Sikorsky's proposal, which was essentially a scaled-up S-61R fitted with twin General Electric T64 turboshaft engines and the dynamic systems of the S-64/CH-54, was selected. On 14 October 1964, the YCH-53A performed its maiden flight; the first deliveries of production CH-53s to operational units commenced on 12 September 1966. The first combat use of the type occurred during the following year when it was deployed to the Vietnamese theater; the CH-53 quickly proved its value for moving heavy payloads, particularly in the recovery of damaged aircraft.
Several variants of the type were promptly introduced. The United States Air Force introduced the HH-53 "Super Jolly Green Giant", configured for special operations and combat search and rescue (CSAR) missions, during the latter part of the Vietnam War; the majority of these were subsequently rebuilt into the MH-53 Pave Low. The visually similar CH-53E Super Stallion is a heavier-lifting improved version of the rotorcraft, designated S-80E by Sikorsky; its third engine makes it more powerful than the Sea Stallion and thus displaced it for the heavy-lift mission. Furthermore, many early-build CH-53s were refitted with more powerful engines, while others were reconfigured for different mission roles, such as US presidential flights, training, and airborne mine countermeasures (AMCM) operations.
Several export deals for the CH-53 were made, leading to several international operators of the type. Among these are Germany, Iran, and Israel. Several unusual or high-profile operations have been undertaken, such as the capture and transportation of a Soviet advanced radar system to Israel under Operation Rooster 53 in 1969, and Iran's capture of five American CH-53s as a result of Operation Eagle Claw in 1980. Various operators deployed their CH-53s during international missions, often under the auspices of NATO or the United Nations, such as for UNSCOM in Iraq, in Kosovo with Kosovo Force (KFOR), Implementation Force (IFOR) in Bosnia and Herzegovina, and the International Security Assistance Force (ISAF) in Afghanistan. While several operators have opted to retain the type into the twenty-first century, many others have opted to supplement or withdraw their Sea Stallions in favor of other platforms, sometimes with the more powerful CH-53E. The CH-53 remains in service with German and Israeli forces, and is one of the largest military helicopters in service. Germany is planning to replace its fleet, as of the 2020s, with the latest version of the twin-rotor CH-47 Chinook. The latest version of the CH-53, the K model King Stallion is in production as of the 2020s entering service with the United States Marine Corps; this is replacing the Super Stallion, itself an upgraded version of Sea Stallion. The heavily upgraded Jolly Green Giant and Pave Low versions of the CH-53 were retired by 2008, flown by the U.S. Air Force for combat search and rescue. Overall, the CH-53 was replaced in many roles by the V-22 Osprey tilt rotor in U.S. service.
In 1960, the United States Marine Corps (USMC) began to seek a replacement for their HR2S piston-powered helicopters. On 27 January 1961, the USMC began working with the U.S. Army, Navy, and Air Force on the "Tri-Service VTOL transport", which would eventually emerge as the LTV XC-142 tiltwing. The design became more elaborate and the program stretched out, causing the USMC to drop out when they decided they would not receive a working machine in a satisfactory timeframe. In particular, there were concerns that the high levels of downwash produced by the XC-142A would render shipborne operations impractical. In the end, the XC-142A, although a very innovative and capable machine, never entered production.
In March 1962, the United States Navy's Bureau of Naval Weapons, acting on behalf of the USMC, issued a request for a "Heavy Helicopter Experimental / HH(X)". The specifications dictated a load capability of 8,000 pounds (3,600 kg) with an operational radius of 100 nautical miles (190 km; 120 mi) at a speed of 150 knots (280 km/h; 170 mph). It was also specified to possess a higher top speed and greater lifting capacity than existing helicopters while also having a lower empty weight than preceding designs as well. The HH(X) was to be used in the assault transport, aircraft recovery, personnel transport, and medical evacuation roles. In the assault transport role, it was to be mostly used to haul heavy equipment instead of troops.
In response, Boeing Vertol offered a modified version of the CH-47 Chinook; Kaman Aircraft offered a development of the British Fairey Rotodyne compound helicopter; and Sikorsky offered what amounted to a scaled-up version of the S-61R, with twin General Electric T64 turboshaft engines and the dynamic system of the S-64/CH-54, to be designated the S-65. Kaman's proposal quickly died when the British government dropped its backing of the Rotodyne program. Competition between Boeing Vertol and Sikorsky was intense, with the Chinook having an advantage because it was being acquired by the United States Army. During July 1962, it was announced that Sikorsky's bid had been selected as the winner on account of various considerations, including cost, technical factors, and production capability. However, a contract was not immediately forthcoming due to budgetary limitations.
The USMC had originally sought to procure four prototypes. However, in light of funding shortfalls, Sikorsky, determined to keep the deal, reduced their estimate for the program's development costs by proposing that development could be performed with only two prototypes. Military officials favorably received the company's proposed reduction; in September 1962, Sikorsky was awarded a $9,965,635 (~$78.9 million in 2024) contract for the production of a pair of YCH-53A prototypes, as well as a mockup and a ground-test airframe.