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Semitoroidal-diaphragm cavitating valve designed for bipropellant flow controlValve controls the flow of bipropellant liquids in rocket engines. Throttling and cavitation of the liquids are controlled by axial deflections of a semitoroidal metal diaphram. The valve is highly resistant to corrosion and leakage, and should be useful in food processing and chemical industries.
Document ID
19690000016
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Young, A. L.
Date Acquired
August 5, 2013
Publication Date
February 1, 1969
Subject Category
Mechanics
Report/Patent Number
XNP-09704
Report Number: XNP-09704
Accession Number
69B10016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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