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Cryogenic gel flow viscometerCoiled section of tubing measures viscous properties of gelled cryogenic propellants under conditions closely resembling flow in rocket engine systems. Characteristic flow curve provides data necessary for the design of prototype hardware systems using the liquid or gel of interest.
Document ID
19720000180
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Globus, R. H. (Aerojet Liquid Rocket Co.)
Vanderwall, E. M. (Aerojet Liquid Rocket Co.)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Physical Sciences
Report/Patent Number
ARC-10523
Report Number: ARC-10523
Accession Number
72B10180
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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