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Flight testing the fixed wing configuration of the Rotor Systems Research Aircraft (RSRA)The Rotor Systems Research Aircraft (RSRA) is a unique research aircraft designed to flight test advanced helicopter rotor system. Its principal flight test configuration is as a compound helicopter. The fixed wing configuration of the RSRA was primarily considered an energy fly-home mode in the event it became necessary to sever an unstable rotor system in flight. While it had always been planned to flight test the fixed wing configuraion, the selection of the RSRA as the flight test bed for the x-wing rotor accelerated this schedule. This paper discusses the build-up to, and the test of, the RSRA fixed wing configuration. It is written primarily from the test pilot's perspective.
Document ID
19860036326
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hall, G. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Morris, P. M.
(U.S. Army, Aeromechanics Laboratory, Moffett Field CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Accession Number
86A21064
Distribution Limits
Public
Copyright
Other

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