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The XV-15 tilt rotor research aircraftThe design characteristics of the XV-15 Tilt rotor research aircraft are presented. Particular attention is given to the following: control system; conversion system; and propulsion system. Flight test results are also reported.
Document ID
19810001546
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dugan, D. C. (NASA Ames Research Center Moffett Field, CA, United States)
Erhart, R. G. (Bell Helicopter Textron Fort Worth, Tex., United States)
Schroers, L. G. (AVRADCOM)
Date Acquired
September 4, 2013
Publication Date
September 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
A-8343
AVRADCOM-TR-80-A-15
NASA-TM-81244
Report Number: A-8343
Report Number: AVRADCOM-TR-80-A-15
Report Number: NASA-TM-81244
Accession Number
81N10054
Funding Number(s)
PROJECT: RTOP 532-04-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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