NASA NTRS · 19750014672
Line Fluid Actuated Valve Development Program
Abstract
The feasibility of a line-fluid actuated valve design for potential application as a propellant-control valve on the space shuttle was examined. Design and analysis studies of two prototype valve units were conducted and demonstrated performance is reported. It was shown that the line-fluid actuated valve concept offers distinct weight and electrical advantages over alternate valve concepts. Summaries of projected performance and design goals are also included.
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Lynch, R. A.. 1975-01-01. Line Fluid Actuated Valve Development Program. https://ntrs.nasa.gov/citations/19750014672
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