The Westland WS-51 Dragonfly helicopter was built by Westland Aircraft and was a license-built version of the American Sikorsky S-51. Apart from military use, it was sold into civilian use.
[edit] Design and development
In December 1946 an agreement was signed between Westland Aircraft and Sikorsky to allow a British version of the S-51 to be manufactured under license in the United Kingdom. These would be powered by the 500 hp Alvis Leonides radial engine. A modified version was also developed by Westland as the Westland Widgeon, but it was unsuccessful.
[edit] Operational history
The Dragonfly entered service with the Royal Navy in 1950 in the air-sea rescue role. A number were also used by the Royal Air Force for casualty evacuation. It was replaced in British service by the Westland Whirlwind, another derivative of a Sikorsky design, in the late 1950s. Fifty-one civilian WS-51s were produced.
[edit] Variants
- Westland/Sikorsky WS-51
- Prototype.
- Dragonfly HR.1
- Air-sea search and rescue helicopter for the Royal Navy powered by a 540 hp (403 kW) Alvis 50 radial piston engine. 13 built, some modified later as HR.5s.
- Dragonfly HC.2
- Casualty evacuation helicopter for the Royal Air Force similar to the commercial Mark 1A, three built.
- Dragonfly HR.3
- Air-sea search and rescue helicopter for the Royal Navy. Similar to the Dragonfly HR.1, but fitted with all-metal rotor blades, 58 built some later modifed as HR.5s.
- Dragonfly HC.4
- Casualty evacuation helicopter for the RAF similar to the Dragonfly HR.3 with all-metal rotor blades, 12 built.
- Dragonfly HR.5
- Air-sea search and rescue helicopter for the Royal Navy similar to the Dragonfly HR.3. Modifed from HR.1 and HR.3.
- Westland-Sikorsky WS-51 Mk.1A
- Civil transport helicopter powered by a 520 hp (388 kW) Alvis Leonides 521/1 radial piston engine. Built by Westland in the United Kingdom.
- Westland-Sikorsky WS-51 Mk.1B
- Civil transport helicopter powered by a 450 hp (336 kW) Pratt & Whitney R-985-134 Wasp Junior radial piston engine.
[edit] Operators
Belgium
Egypt
France
Iraq
Italy
Ceylon
Japan
Thailand
United Kingdom
Yugoslavia
[edit] Survivors
[edit] Specifications (Dragonfly HR.1)
Data from [1]
General characteristics
- Crew: 1 (pilot)
- Capacity: 3 (passengers)
- Length: 57 ft 6½ in (17.54 m)
- Main rotor diameter: × 48 ft 0 in (14.63 m)
- Height: 12 ft 11½ in (3.95 m)
- Main rotor area: 1809.56 ft² (168.11 m²)
- Empty weight: 4380 lb (1987 kg)
- Gross weight: 5870 lb (2663 kg)
- Powerplant: 1 × Alvis Leonides 50 radial piston, 540 hp (403 kW)
Performance
- Maximum speed: 95 mph (153 km/h)
- Range: 300 miles (483 km)
- Service ceiling: 12,400 ft (3780 m)
[edit] See also
Related development
Related lists
[edit] References
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
[edit] External links
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