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Flight testing the Rotor Systems Research Aircraft (RSRA)The Rotor Systems Research Aircraft (RSRA) is a dedicated rotor test vehicle whose function is to fill the gap between theory, wind tunnel tests and flight verification data. Its flight test envelope has been designed to encompass the expected envelopes of future rotor systems under all flight conditions. The test configurations of the RSRA include pure helicopter and compound (winged helicopter) modes. In addition, should it become necessary to jettison an unstable rotor system in flight, the RSRA may be flown as a fixed wing aircraft. The heart of the RSRA's electronic flight control system is the TDY-43 computer, which can be programmed in numerous ways to change stability and control or force feel system gains. Computer programming changes allow the RSRA to be used as a five-degree-of-freedom inflight simulator for studying the handling qualities of research rotors.
Document ID
19840033210
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Merrill, R. K.
(U.S. Army, Aviation Engineering Flight Activity, Edwards AFB CA, United States)
Hall, G. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Stability And Control
Accession Number
84A15997
Distribution Limits
Public
Copyright
Other

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