NASA NTRS · 19730000207
Mass flow controller for gaseous propellants
Abstract
Gaseous 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.
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1973-06-01. Mass flow controller for gaseous propellants. https://ntrs.nasa.gov/citations/19730000207
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