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Monitor for physical property changes in solid propellantsSpecially designed sensor is attached to or imbedded in propellant. When sensor is driven into vibration, it moves with a phase lag directly proportional to internal friction or loss coefficent. Resonance frequency of the system is related to Young's modulus. Modulus or internal friction can be monitored over long period of time.
Document ID
19730000130
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Black, R. E., Jr.
(Thiokol Chemical Corp./Elkton Div.)
Date Acquired
August 7, 2013
Publication Date
March 1, 1973
Subject Category
Physical Sciences
Report/Patent Number
ARC-10702
Report Number: ARC-10702
Accession Number
73B10130
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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