Bell HSL

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HSL (Bell Model 61)
U.S. Navy HSL-1 61.jpg
The U.S. Navy Bell XHSL-1 prototype in flight.
RoleTandem-rotor ASW helicopter
National originUnited States
Manufacturer Bell Helicopter
First flight3 March 1953
Introduction1957
Retired1960
StatusRetired
Primary user United States Navy
Number built53 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. It had its first flight in 1953 and entered service with the U.S. Navy in 1957. Over 50 models were produced but it was out of service by 1960 such was the pace of helicopter development in this period.

Contents

The helicopter had two main rotors at either end of the fuselage tube, linked by a transmission but powered by a single Pratt & Whitney R-2800-50m, which was an 18-cylinder air-cooled radial engine. The front rotor shaft was actually slightly ahead of pilots in the front cockpit.

Design and development

XHSL-1 prototype on a test flight Bell XHSL-1 prototype in flight c1953.jpg
XHSL-1 prototype on a test flight

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.

Operational history

HSL-1 in a hover over water Bell HSL-1 hovering.jpg
HSL-1 in a hover over water
HSL-1 towing test Bell HSL-1 towing tests 1956.jpg
HSL-1 towing test

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.

Variants

XHSL-1
two experimental flight test and one static test article
HSL-1
production version, 50 built.
Bell Model 61
Company designation for the HSL
Bell D-116
A proposed civil variant of the Model 61, not proceeded with.
Bell D-216
A proposed variant of the HSL, not proceeded with.
Bell D-238
A proposed variant of the HSL, not proceeded with.

Operators

Flag of the United States (23px).png  United States

Specifications (HSL-1)

3-view line drawing of the Bell HSL-1 Bell HSL-1 3-view line drawing.png
3-view line drawing of the Bell HSL-1

Data from NAVAER-1519B - Bell HSL-1 :Characteristic Summary [3] Bell Aircraft since 1935 [4] <

General characteristics

16,853 lb (7,644 kg) (attack mission)
normal power at sea level, 1,900 hp (1,417 kW) at 2,400 rpm

Performance

1,200 ft/min (6.1 m/s) in vertical flight with take-off power, sea level, at take-off weight in forward flight

Armament

Avionics

See also

Aircraft of comparable role, configuration, and era

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References

Notes
  1. Hearst Magazines (August 1953). "Navy's Most Powerful Helicopter to Hunt Submarines". Popular Mechanics. Hearst Magazines. p. 121.
  2. "Flight 1956 pg.518". flightglobal.com. Retrieved 18 October 2014.
  3. NAVAER-1519B - Bell HSL-1 :Characteristic Summary (Revision 10-51 ed.). Navaer. 30 August 1958.
  4. Pelletier, Alain J. (1992). Bell Aircraft since 1935 (1st ed.). London: Putnam & Company Ltd. pp. 100–102. ISBN   1-55750-056--8. OCLC   25625769.
Bibliography