NASA NTRS · 19910000598
Pressure-Actuated Flow-Control Valve
Abstract
Flow-control valve varies cross-sectional area with drop in pressure. Conceived for controlling flow of oxidizing fluid in rocket engine, concept applicable to other situations necessary to vary flows over wide ranges. In rocket-engine application, fluid liquid or gaseous, depending on chosen operating conditions.
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Cox, George B., Jr.. 1991-11-01. Pressure-Actuated Flow-Control Valve. https://ntrs.nasa.gov/citations/19910000598
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