Bibliography on Clean Rooms
Bibliography on contamination control, and air filtering for application to electronics and surgical instruments
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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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Bibliography on contamination control, and air filtering for application to electronics and surgical instruments
K lubricated journal bearings materials friction and wear over temperature range in sliding contact in liquid K and high vacuum
Fracture toughness and mechanical properties of titanium alloys at cryogenic temperatures for booster tank applications
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Load and temperature effects on fatigue strength of notched titanium alloy sheet for supersonic transport operation
Adaptation schedule for human coriolis effect in slow acceleration steps
High pressure storage vessels for gaseous hydrogen, discussing failure, manufacturing controls and access for internal nondestructive inspection
Human reactions to coriolis effect in rotating environments
Stress induced dimensional changes in glass mirror surfaces
Adaptation to Coriolis accelerations associated adaptation schedule to with 1-rpm increments developed for preventing motion sickness in slow rotating environment
Hydrogen, N, O, Kr methane and carbon dioxide gas chromatographic examination, discussing life detection device for Mars landing
Transfer functions for calculating coupled acoustic/elastic response of structure to sonic boom
Numerical analysis of Helmholtz resonator system established between windows and open doors when subjected to sonic boom impulsive loads
Mechanical property tests of nickel, titanium, and iron alloys in 5000 psig gaseous helium and hydrogen at various temperatures
Experimental efforts in this program for this period. Mechanical property tests of wrought and cast nickel-base alloys and one wrought cobalt-base alloy were conducted in 34.5 MN/sq m (5000-psig) helium and hydrogen or hydrogen mixtures. Comparison of test results was made to determine degradation of properties due to the hydrogen environments. All testing was conducted on solid specimens exposed to external gaseous pressure. Specific mechanical properties determined and the testing methods used are summarized.
Superalloys are being considered for the primary heat shields and supports in the thermal protection system of both hypersonic transport and space shuttle vehicles. Since conservative design philosophy dictates designs based on residual material properties at the end of the service life, material characterization after exposure to the environmental conditions imposed by the flight requirements of these two classes of vehicles is needed on the candidate alloys. An investigation was conducted to provide some of the necessary data, with emphasis placed on oxidation, creep, and residual properties of thin-gage sheet material.
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It was concluded that thermally activated relaxation of the type customarily encountered at high temperatures was not expected to occur at the low temperatures where long time NERVA storage conditions will prevail. Instances where relaxation occurred by a different mechanism at such moderate temperatures were also reported. Twelve simulated bolted flange test specimens were prepared. Parameters that were varied among the twelve specimens were the flange material, the bolt shank diameter, and the bolt loading in terms of percent of yield strength.