The Bell XH-15, also called the Bell Model 54, was a utility helicopter built in the United States by Bell Helicopter in the late 1940s. It was designed to meet a requirement for a liaison and utility helicopter for the United States Army and the United States Air Force. The Model 54 used a conventional pod and boom layout with fixed tricycle landing gear, and a single piston engine mounted in the rear cabin drove one two-bladed rotor. The Army Air Forces ordered three examples in February 1946 as the XR-15, and the type flew for the first time in March 1948 under the new designation XH-15. After evaluation by the Air Force no production orders followed and the project ended in 1950, so the XH-15 stayed a prototype programme.
Facts
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Exemplifies
Source Bell XH-15 (Wikipedia)
Of Make
Source Bell XH-15 (Wikipedia)
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Manufactured By
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Source Bell XH-15 (Wikipedia)LeadQuote, Lead
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.
Originated In
Also in Geography Atlas: where this subject originated.
Source Bell XH-15 (Wikipedia)LeadQuote, Lead
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.
Sources
1. Bell XH-15 (Wikipedia)
Lead
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.
Development, first flight
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.
Development, outcome
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.
Development, powerplant
Continental XO-470-5 piston engine located in the rear cabin
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