Sikorsky CH53

HititAir Sikorsky CH-53 (Alpha Sim)

(please click on picture for texture )

Sikorsky
Sikorsky

 

 

Sikorsky CH-53

The CH-53 Sea Stallion is the most common name for the Sikorsky S-65 family of heavy-lift transport helicopters. Originally developed for use by the United States Marine Corps, it is also in service with Germany, Mexico, Iran, Israel, and as the MH-53 Pave Low with the United States Air Force. The USAF also operated the HH-53 "Super Jolly Green Giant" during the late- and post-Vietnam War era.

The dimensionally-similar CH-53E Super Stallion is a heavier-lifting, improved version designated S-80E by Sikorsky. Its third engine makes it more powerful than the Sea Stallion, which it has replaced in the heavy-lift mission.

In 1960, the US Marine Corps began to seek a replacement for their old S-56 piston-powered helicopters, originally working with the other three U.S. armed services on the "Tri-Service VTOL transport", which would eventually emerge as the Vought-Hiller-Ryan XC-142A tilt-wing. The design became more elaborate and the program stretched out resulting in Marines deciding they couldn't get a workable machine in a satisfactory timeframe and dropped out. This was just as well, because the XC-142A, although a very innovative and capable machine, would never enter production.

In March 1962, the US Navy Bureau of Weapons, acting on behalf of the Marines, issued a request for a "Heavy Helicopter Experimental / HH(X)". The specifications dictated a load capability of 8,000 pounds (3,630 kilograms) with an operational radius of 100 NM (185 km) at a speed of 150 kt (278 km/h). 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 Chinook; Kaman 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 GE T64 turboshafts and the dynamic system of the S-64, 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 Boeing Vertol having something of an edge because the type was being acquired by the U.S. Army. Sikorsky threw everything into the contest and was awarded the contract in July 1962.

The Marines originally wanted to buy four prototypes but ran into funding problems. Sikorsky, determined to keep the deal, cut their estimate for development costs and said that the program could be done with two prototypes. The military bought off on the proposal, and in September 1962 Sikorsky was awarded a contract for a little under US$10 million for two "YCH-53A" prototypes, as well as a mockup and a ground-test airframe.

The development program did not go entirely smoothly, due to a shortage of engineering resources plus various failures of subcontractors and the government, but these problems were gradually overcome. There was also the problem that U.S. Defense Secretary Robert S. McNamara was pushing "commonality" between the armed services and pressuring the Marines to obtain the Chinook anyway, but the Marines managed to convince McNamara's people that the Chinook couldn't meet requirements without a lot of expensive changes.

All these obstacles overcome, the first YCH-53A performed its initial flight at the Sikorsky plant in Stratford, Connecticut, on October 14, 1964, about four months behind schedule. The Marines had already placed an initial production contract for 16 helicopters in September. Flight trials went more smoothly than expected, helping make up for the lost time in development. It received the military designation and name "CH-53A Sea Stallion". Delivery of production CH-53s began in 1966.

The CH-53A arrived in Vietnam in January 1967 and proved useful, eventually recovering even more downed aircraft than the CH-54. A total of 141 CH-53As were built, including the two prototypes. The US Navy acquired 15 CH-53As from the USMC in 1971 for airborne mine countermeasures (AMCM) activities. The helicopters had more powerful T64-GE-413 turboshafts installed and the received the designation "RH-53A".

The USAF ordered the HH-53B in September 1966 and first flew on March 15, 1967. It added a refueling probe, drop fuel tanks and a rescue hoist and featured upgraded T64-GE-3 engines. The Air Force used the HH-53B for combat search and rescue (CSAR). HH-53C was an improved CSAR variant with a smaller 450 US gallon (1,705 liter) for improved performance. It also added more armor and better communication systems. The CH-53C was similar except it lacked a refueling probe. It was used by the USAF for more general transport work.

Heavy lifting in tropical climates demanded more power so the Marines decided to acquire an improved variant, the "CH-53D", with uprated engines, originally the T64-GE-412 then later the T64-GE-413. The CH-53D also included an uprated transmission to go with the more powerful engines, and a revised interior to permit a load of 55 troops.

The initial flight of the CH-53D was on January 27, 1969. The CH-53D served alongside the CH-53A through the rest of the Vietnam War. A VIP transport version designated, "VH-53D" with plush accommodations was used by the Marines for the US presidential flights. The US Navy also acquired CH-53D based helicopters for mine sweeping. These were designated "RH-53D" and included mine sweeping gear such as a pair of Browning 0.50 in (12.7 mm) machine guns for detonating mines. The Navy received 30 RH-53Ds beginning in 1973. After the RH-53Ds were in service, the RH-53As were handed back to the Marines and restored to CH-53A configuration.

During the 1980s, Israeli Air Force's CH-53 Yas'ur fleet was upgraded and improved by Israel Aircraft Industries, along with military high-tech firm Elbit Systems. The project – which ended only in 1997 – improved the CH-53 avionics, robustness and extended its life span by at least two decades.

In 1989, some of the CH-53As being retired by the Marines were passed on to the U.S. Air Force for training, with these helicopters redesignated "TH-53As". The TH-53As were stripped of most operational equipment and painted in USAF camouflage colors.

General characteristics

  • Crew: 2 Pilots, 1 or more Crew Chiefs
  • Capacity: 37 troops (55 in alternate configuration) or 24 stretchers
  • Length: 88 ft 6 in (26.97 m)
  • Rotor diameter: 72 ft 2.7 in (22.01 m)
  • Height: 24 ft 11 in (7.6 m)
  • Empty weight: 23,628 lb (10,740 kg)
  • Loaded weight: 33,500 lb (15,227 kg)
  • Powerplant:General Electric T64-GE-413 turboshafts, 3,925 shp (2,927 kW) each
  • Width (overall): 28 ft 4 in (8.64 m)
  • Width (fuselage): 15 ft 6 in (4.7 m)
  • Maximum takeoff (Internal Load): 69,750 lb (31,666 kg)
  • Maximum takeoff (External Load): 73,500 lb (33,369 kg)
  • Rotor systems: 6 blades on main rotor

Performance

 

 

Cockpit
CH53
 
HititAir