HSL (Bell Model 61) | |
---|---|
The U.S. Navy Bell XHSL-1 prototype in flight. | |
Role | Tandem-rotor ASW helicopter |
National origin | United States |
Manufacturer | Bell Helicopter |
First flight | 3 March 1953 |
Introduction | 1957 |
Retired | 1960 |
Primary user | United States Navy |
Number built | 53 including one static test article |
The Bell HSL (Model 61) was an American 1950s anti-submarine warfare (ASW) helicopter built by the Bell Helicopter company, the only tandem rotor type designed by Bell.
The prototype Bell Model 61 first flew on 3 March 1953; it had been designed to meet a United States Navy requirement for an anti-submarine warfare helicopter. In June 1950, the Model 61 was announced as the winner of the competition, and three XHSL-1 evaluation aircraft were ordered. The Model 61 had a rectangular-section fuselage structure and four-leg, six-wheel landing gear. It was powered by a Pratt & Whitney R-2800 radial engine mounted in the aft fuselage. Crew included two pilots and two sonar operators. [1]
Because of the urgency of the requirement, low-rate production was ordered almost immediately after Bell received a contract for three XHSL-1s. The Navy eventually contracted for at least 160 production aircraft, including 18 intended for the British Royal Navy. Bureau Numbers were assigned for a total of 234. Because of development problems that resulted in poor schedule performance to the contract, only 50 were built. Although all were delivered, after service test and acceptance only a handful were used, for the development of airborne mine sweeping. The rest were delivered directly into storage and were subsequently struck off.
The HSLs were not used operationally. Approximately seven were assigned to the U.S. Naval Air Mine Defense Unit at Panama City, Florida, for the development of airborne mine-sweeping, the first arriving in September 1956 and the last being struck off in early 1960.
Data from NAVAER-1519B - Bell HSL-1 :Characteristic Summary [3] Bell Aircraft since 1935 [4] <
General characteristics
Performance
Armament
Avionics
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