Sikorsky S-62

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Sikorsky S-62
A USCG HH-52A Seaguard landing on an icebreaker
Type SAR/utility helicopter
Manufacturer Sikorsky Aircraft
Maiden flight 1959
Introduced 1961
Primary user United States Coast Guard

The Sikorsky S-62 is a single turbine engine, single rotor amphibious helicopter originally developed as a commercial venture by the Sikorsky Aircraft Corporation of Stratford, Connecticut. It was used by the Coast Guard primarily for search and rescue, and now has been replaced by non-amphibious types such as the HH-65 Dolphin which rely on using a winch to retrieve passengers from a hover.

Contents

[edit] History

A number of aircraft were bought by the US Navy Bureau of Aeronautics for the US Coast Guard for use as a search and rescue helicopter and designated the HU2S-1G Seaguard. The HU2S-1G was re-designated the HH-52A Seaguard in 1962.

The HH-52A used a boat hulled shaped fuselage, smaller but similar to the US Navy's SH-3 (Sikorsky S-61), and was employed aboard the larger Coast Guard cutters and icebreakers. The S-62 used a single 1250 hp General Electric T58-GE-8 turboshaft engine, the same powerplant used on the larger twin-engined SH-3.

The turbine powered S-62 could carry more weight and fly faster than the H-19 (S-55). The aircraft was first conceived and designed to be amphibious so that flotation gear would not be required for over water flights, and rescues could be made by landing on the water. The fuselage is watertight for landings on water or snow. Two outrigger floats resist pitching and rolling on the water. Although the HH-52A looks very different from the Sikorsky H-19, it used many of the same components.

[edit] Variants

  • S-62 : Prototype.
  • S-62A : Amphibious transport helicopter. The S-62A was the first production version.
  • S-62B : One S-62 was fitted with the main rotor system of the S-58.
  • S-62C : Company designation of the HH-52A search and rescue helicopter for the United States Coast Guard.

[edit] Operators

[edit] Military operators

[edit] Specifications (HH-52A)

General characteristics

  • Crew: 3
  • Length: 44 ft 7 in (13.57 m)
  • Rotor diameter: 53 ft (16.16 m)
  • Height: 14 ft 2 in (4.33 m)
  • Empty weight: 4,956 lb (2,248 kg)
  • Useful load: 3,047 lb (1,382 kg)
  • Max takeoff weight: 8,003 lb (3,630 kg)
  • Powerplant:General Electric T58-GE-8 turboshaft, 1250 shp derated to 730 shp (500 kW)

Performance

[edit] Related content

Related development

 

Designation sequence

[edit] External links

[edit] Notes

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