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Bell XH-15





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The Bell XH-15 (Bell Model 54) was an American two-seat utility helicopter designed and built by Bell Helicopter, to meet a requirement for a liaison and utility helicopter for the United States Army and United States Air Force.

XR-15/XH-15
Role Four-seat utility helicopter
National origin United States
Manufacturer Bell Helicopter
First flight 1948
Status Canceled
Primary user United States Air Force
Number built 3

Development

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The Model 54 was a conventional pod-and-boom four-seat helicopter with wheeled, fixed tricycle landing gear, powered by a single 275 hp Continental XO-470-5 piston engine located in the rear cabin, driving a single two-bladed rotor. The United States Army Air Forces (USAAF) ordered three in February 1946 as the XR-15. The first flight was made in March 1948 with the new designation XH-15, but no orders were forthcoming following evaluation by the United States Air Force (USAF) and the project ended in 1950.

Variants

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XR-15
Military designation for three Model 54s ordered for evaluation.[1]
XH-15
XR-15 redesignated before delivery.[1]

Operators

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  United States

Specifications

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General characteristics

Performance

See also

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Related lists

References

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Notes

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  1. ^ a b Andrade 1979, p. 162

Bibliography

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Retrieved from "https://en.wikipedia.org/w/index.php?title=Bell_XH-15&oldid=1154001103"
 



Last edited on 9 May 2023, at 16:34  





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This page was last edited on 9 May 2023, at 16:34 (UTC).

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