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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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Protective coating parameters for improving oxidation resistance and reliability of silicide coating systems for tantalum alloys
Hypervelocity heat protection, surface heat shielding, and internal temperature rise of Teflon, phenolic nylon, epoxy resin in glass honeycomb, and silicone elastomer
Systems analysis of electrical grounding system for lightning protection of STADAN
Ablative thermal protection system for X-15 aircraft operating at hypersonic speeds
Flight test and performance analysis of ablative thermal protection system for X-15A-2 aircraft
Space radiation transport, spacecraft shielding design and advanced concepts, and methods for calculating radiation penetration through protective shields - conference
Heat resistant protective coatings for use in liquid propellant rocket engines
High temperature protective coatings of iridium on tantalum, niobium, molybdenum, and tungsten
Premature actuation protection against RF interference for electroexplosive devices in spacecraft pyrotechnic systems
Refractory metal coatings protective capabilities in rocket engine propulsive environment evaluated for effectiveness
Study establishes the quality of chemical and galvanized protection afforded by anodized and aldozided coatings applied to test panels of various aluminum alloys. The test panels, placed in firm contact with panels of titanium alloys, were subjected to salt spray tests and visually examined for corrosion effect.
Effectiveness of conversion coatings designed to protect aluminum alloys against atmospheric corrosion is reduced after exposure to high temperature or welding. Damaged coating should be manually stripped six inches from the weld and then recoated by sponge or spray with the original solution.
Two suits of protective clothing reduce hazards to personnel working near short-arc lamps. One suit is worn during assembly or servicing of inoperative 5- and 20-kw lamps. The other suit is worn during adjustment or focusing of operating 5-kw lamps.
Shadow shields for thermal protection of cryogenic tanks in space
Silicide coatings for oxidation protection of tantalum and niobium
Parametric study of optimized liquid hydrogen thermal protection systems for nuclear interplanetary spacecraft
Technical analyses and computer programs in support of optimization of liquid hydrogen thermal protection systems for nuclear Mars spacecraft
Data tables for optimal thermal protection of liquid hydrogen storage in nuclear interplanetary spacecraft