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Colloidal suspension simulates linear dynamic pressure profileMissile nose fairings immersed in colloidal suspension prepared with various specific gravities simulate pressure profiles very similar to those encountered during reentry. Stress and deflection conditions similar to those expected during atmospheric reentry are thus attained in the laboratory.
Document ID
19660000213
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mc Cann, R. J.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Mechanics
Report/Patent Number
WOO-266
Report Number: WOO-266
Accession Number
66B10214
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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