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Rotor systems research aircraft: Fixed-wing simulations resultsThe setup, validation, and results of the Rotor Systems Research Aircraft (RSRA) fixed-wing, moving-base simulation performed in May 1983 are covered. The emphasis of the simulation was to familiarize the pilots with the RSRA's fixed-wing configuration. Additional information concerning stall speeds, minimum control speed, and various gross weights were recorded and included in the report.
Document ID
19840005108
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kufeld, R. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-85863
NAS 1.15:85863
A-9549
Report Number: NASA-TM-85863
Report Number: NAS 1.15:85863
Report Number: A-9549
Accession Number
84N13176
Funding Number(s)
PROJECT: RTOP 532-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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