Accession Number : AD0801716
Title : SECONDARY PRESSURE REGULATOR TESTS.
Descriptive Note : Final rept.,
Corporate Author : LOCKHEED MISSILES AND SPACE CO INC SUNNYVALE CA
Personal Author(s) : Reinthaler, C. R.
Report Date : 14 JUN 1958
Pagination or Media Count : 13
Abstract : Previous testing on proposed models of a secondary pressure regulator had indicated the need for additional development. Earlier tests with the unit revealed trouble with the valve seat and the diaphragm. The aluminum alloy seat proved susceptible to erosion as a result of high velocity flow which in turn permitted excessive leakage. Consequently the supplier submitted for evaluation a regulator with a stainless steel seat and a change in diaphragm material from silicon rubber to teflon impregnated fiberglas. The results of that evaluation form the basis of this report.
Descriptors : (*PROPELLANT TANKS, PRESSURE REGULATORS), ACCEPTABILITY, OPERATION, VALVES, DIAPHRAGMS(MECHANICS), ALUMINUM ALLOYS, EROSION, LEAKAGE(FLUID), STAINLESS STEEL, SYNTHETIC RUBBER, SILICONES, GLASS TEXTILES, HALOCARBON PLASTICS, FLUORINE COMPOUNDS, IMPREGNATION, FLUID FLOW, PRESSURIZATION, VIBRATION, ACCELERATION.
Subject Categories : Containers and Packaging
Distribution Statement : APPROVED FOR PUBLIC RELEASE