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Flight Experience With Lightweight, Low-Power Miniaturized Instrumentation SystemsEngineers at the NASA Dryden Flight Research Facility (NASA-Dryden) have conducted two flight research programs with lightweight, low-power miniaturized instrumentation systems built around commercial data loggers. One program quantified the performance of a radio-controlled model airplane. The other program was a laminar boundary-layer transition experiment on a manned sailplane. The purpose of this paper is to report NASA-Dryden personnel's flight experience with the miniaturized instrumentation systems used on these two programs. The paper will describe the data loggers, the sensors, and the hardware and software developed to complete the systems. The paper also describes how the systems were used and covers the challenges encountered to make them work. Examples of raw data and derived results will be shown as well. Finally, future plans for these systems will be discussed.
Document ID
19930027283
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Philip J Hamory
(Dryden Flight Research Facility Edwards, California, United States)
James E Murray
(Dryden Flight Research Center Rosamond, California, United States)
Date Acquired
August 15, 2013
Publication Date
August 24, 1992
Publication Information
Publication: 6th AIAA Biennial Flight Test Conference
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
AIAA-92-4111
Meeting Information
Meeting: 6th AIAA Biennial Flight Test Conference
Location: Hilton Head, SC
Country: US
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
93A11280
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Flight Testing
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