Suit glove advanced thermal protection program Final report
Design and performance of extravehicular astronaut thermal protection gloves
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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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Design and performance of extravehicular astronaut thermal protection gloves
Dynamic response of thermal protection system panel for space shuttle
Criteria and procedures for determining dosage of penetrating space radiation and design of appropriate protection for space vehicles
Metalliding parameters developed for sequential deposition of manganese, aluminum, and tantalum alloys as protective coatings for superalloys
Entry trajectory control effects on thermal protection system weight of space shuttle
Structure of fabric layers for micrometeoroid protection garment with capability for eliminating heat shorts for use in manufacturing space suits
Production engineering and chemical, mechanical, and thermodynamic properties of thoria dispersed nickel chrome alloys for space shuttle thermal protection applications
Circuit design for failure sensing and protecting low voltage electric generator and power transmission networks
Protective coating of phosphate-bonded zirconia for regeneratively cooled thrust chambers
Development of method for protecting large and oddly shaped areas from radiant and convective heat
Determination of oxidation resistance of various alloys for possible application as thermal control and protection system components on space shuttles
Development of reusable oxidation resistant carbon-carbon laminates and surface insulation materials for thermal protection systems
Creep analysis of metallic thermal protection system under simulated mission environments
Light weight, low cost, ablative thermal protection system for space shuttles
Launch vehicle thermal protection system evaluation based on thermal and pressure distributions over exposed booster surface
Active and passive thermal protection system weights for delta body space shuttle for crossrange up to 1500 n.mi.
Environmental simulation testing and evaluation of shuttle thermal protection materials and systems
Polyisocyanurate foam and intumescent paint for thermal protection of aircraft passengers in ground accident fires