NASA NTRS · 19670000074
Flow-test device fits into restricted access passages
Abstract
Test 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.
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Fitzgerald, J. J., Oberschmidt, M., Rosenbaum, B. J.. 1967-04-01. Flow-test device fits into restricted access passages. https://ntrs.nasa.gov/citations/19670000074
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