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.
Pressure-Actuated Flow-Control Valve
NASA Tech Briefs ; 15 , 11
1991-11-01
Sonstige
Keine Angabe
Englisch