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Total main rotor isolation system analysisThe requirements for a preliminary design study and verification procedure for a total main rotor isolation system at n/rev are established. The system is developed and analyzed, and predesign drawings are created for an isolation system that achieves over 95 percent isolation of all six degrees of freedom.
Document ID
19810018538
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Halwes, D. R.
(Textron Bell Helicopter Fort Worth, TX, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-165667
Report Number: NASA-CR-165667
Accession Number
81N27076
Funding Number(s)
CONTRACT_GRANT: NAS1-16211
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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