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Performance of some miniature pressure transducers subjected to high rotational speeds and centripetal accelerationsThe performance characteristics of several miniature pressure transducers were determined at centripetal accelerations up to 11,200 g's at a rotational speed of 23,000 rpm. The variation in centripetal acceleration was produced by changing radial position of the transducer relative to the center of rotation. Residual zero outputs and transducer sensitivities were determined at 23,000 rpm and compared with those determined at 0 rpm. The actual pressures at the various transducer locations differ from the center line impressed pressures due to a rotational effect. Corrections for this effect were made. A brief description of the test apparatus is included.
Document ID
19760011318
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Minkin, H. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-X-71791
E-8643
Report Number: NASA-TM-X-71791
Report Number: E-8643
Meeting Information
Meeting: Intern. Instr. Symp.
Location: San Diego, CA
Country: United States
Start Date: May 25, 1976
End Date: May 27, 1976
Sponsors: Instr. Soc. of Am.
Accession Number
76N18406
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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