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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 577 records · Page 32

Two-step rocket engine bipropellant valve concept

Initiating combustion of altitude control rocket engines in a precombustion chamber of ductile material reduces high pressure surges generated by hypergolic propellants. Two-step bipropellant valve concepts control initial propellant flow into precombustion chamber and subsequent full flow into main chamber.

Capps, J. E.↗

Relief valve

Relief valve to permit slow and fast bleeding rates at difference pressure levels

Steenken, J.↗

Novel valve for reciprocating compressors - Concept

Thin ring valve for the inlets and exhausts of reciprocating compressors, and possibly for the inlets of internal combustion engines, encircles the cylinder and operates on the Bernoulli principle.

Wagner, C. E.↗

An electrothermally actuated micro valve

Microminiature slide action valve requires power only during actuation and can be used as an on-off or single inlet to alternately selected outlets.

Charlton, K. W.↗

Fast-acting, four-way slide valve

Valve is insensitive to fluctuating sense pressure. It remains in full-open position until the supply pressure is removed.

Absalom, J.↗