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Mass flow controller for gaseous propellantsGaseous propellants exhibit large variations in pressure and temperature and hence in fuel delivery. All-mechanical, mass flow controller which compensates for these variations has been developed to maintain constant fuel rate of gas. Further work is necessary to ease inlet pressure limitation.
Document ID
19730000207
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Date Acquired
August 7, 2013
Publication Date
June 1, 1973
Subject Category
Mechanics
Report/Patent Number
MSC-14221
Report Number: MSC-14221
Accession Number
73B10207
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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