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The Second Generation High Speed Rotor Head Mounted Instrumentation SystemNASA Ames Research Center has been investigating the air pressure flow of a rotor blade on a UH-60 Black Hawk helicopter in-flight. This paper will address the changes and improvements due to additional restrictions and requirements for the instrumentation system. The second generation instrumentation system was substantially larger and this allowed greatly improved accessibility to the components for ease of maintenance as well as improved gain and offset adjustment capabilities and better filtering.
Document ID
20020041761
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Lewis, John
(NASA Ames Research Center Moffett Field, CA United States)
Reynolds, R. S.
Date Acquired
August 20, 2013
Publication Date
January 1, 1997
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: Instrument Society of America 43rd International Instrumentation Symposium
Location: Orlando, FL
Country: United States
Start Date: May 4, 1997
End Date: May 8, 1997
Sponsors: Instrument Society of America
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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