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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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Theoretical analysis of five composite ablation materials with various percentages of phenolic resin, powdered nylon, and silica
Thermophysical property measurements on ablative materials for Apollo spacecraft propulsion system configuration
Emittance as function of temperature for five ablative materials used as rocket engine liners
Polybenzimidazole synthesis, ablative screening tests, and char formation in PBI composites
Environmental and ablative materials performance affecting heat shielding requirements of slender and blunt vehicles during hyperbolic reentry
Calculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry vehicles
Analyses and finite difference procedure for predicting transient in-depth response of charring ablation materials
Thermal analysis on pyrolysis of charring ablator materials
Design, operation and construction of event recorder for monitoring heat ablation data
Flight test and performance analysis of ablative thermal protection system for X-15A-2 aircraft
Rotation effects on melting ablation on reentry of axisymmetric bodies
Nucleonic measurement of ablative heat shield material recession
Ballistic range boundary layer transition data on ablating plastic cones
Ablation properties and luminosity of artificial meteoroid materials determined in plasma jet tests
Composite material development and structural design of improved throat inserts for ablative thrust chambers
Reentry shielding ablation measured by imbedded radioactive isotopes with radiation dector
Improved ablative materials - design of chemical vapor plating reactor for preparing titanium boride and titanium carbide continuous filaments
Comparative evaluation of ablative materials in arc jet plasmas