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Research requirements to reduce civil helicopter life cycle costThe problem of the high cost of helicopter development, production, operation, and maintenance is defined and the cost drivers are identified. Helicopter life cycle costs would decrease by about 17 percent if currently available technology were applied. With advanced technology, a reduction of about 30 percent in helicopter life cycle costs is projected. Technological and managerial deficiencies which contribute to high costs are examined, basic research and development projects which can reduce costs include methods for reduced fuel consumption; improved turbine engines; airframe and engine production methods; safety; rotor systems; and advanced transmission systems.
Document ID
19780021139
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blewitt, S. J.
(Boeing Vertol Co. Philadelphia, PA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1978
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-145379
Report Number: NASA-CR-145379
Accession Number
78N29082
Funding Number(s)
CONTRACT_GRANT: NAS1-13624
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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