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Flow-test device fits into restricted access passagesTest device using a mandrel with a collapsible linkage assembly enables a fluid flow sensor to be properly positioned in a restricted passage by external manipulation. This device is applicable to the combustion chamber of a rocket motor.
Document ID
19670000074
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Fitzgerald, J. J.
Oberschmidt, M.
Rosenbaum, B. J.
Date Acquired
August 3, 2013
Publication Date
April 1, 1967
Subject Category
Electronic Components And Circuits
Report/Patent Number
MSC-1078
Report Number: MSC-1078
Accession Number
67B10074
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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