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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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Commercially available ablation materials for use as thermal protection for sidewalls of advanced air-to-air missiles - protective coatings for structures in separated flow region
Analytical model for predicting transient one- dimensional thermal performance of charring- ablator heat-protection system exposed to hyperthermal environment
Evaluation and erosion of nonmetallic ablating materials as rocket nozzle sections
Radioactive isotope technique for heat shield ablation measurement during reentry
Effects of processing and fabrication techniques on properties of composite ablative materials
Ablative material evaluation for nozzle sections of storable propellant rocket engine
Trajectory and ablation characteristics calculation for glass-tipped blunt bodies in atmospheric entry
Three-dimensional, reinforced fabric construction for ablating materials
Meteoroid impact damage to Apollo and Gemini ablative heat shields
Techniques for rating performance of ablative materials in liquid-propellant rocket engines
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal parameters of ablative reentry vehicle heat shield
Lifetime, reliability, and radiation spectrum of ablative flash lamp for Apollo command service module
Effects of thermal-property variations on performance of charring ablator
Analytical study of diffusion-controlled char oxidation and effect on steady state ablation of plastic materials
Exploratory investigation of nylon grain size effect on ablation of phenolic nylon
Ablating materials tested at combined radiative and convective heating for manned reentry vehicle heat shields
Resin systems investigated for improving ablative materials for use with fluorine-containing liquid propellant systems
Laboratory determinations of thermophysical properties of ablative materials