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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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Comparison of foamed radiating materials with composite charring materials to evaluate their ablation and radiation properties for application to thermal protection for manned space vehicles
Free flight tests of subliming ablators and transpiration cooling as thermal protection at hypersonic speeds
Effect of simulated ablation gas injection on shock layer of blunt bodies at Mach 3 and 5
Viscoelastic analysis of structural integrity of accelerated ablating rocket
Radioisotopic continuous measurement techniques for determination of heat shield ablation and sublimation
Passive temperature control coatings for Apollo spacecraft ablative thermal protection system
Attached and separated boundary layers on highly cooled, ablating and nonablating models at Mach 13.8
Hypersonic trim angle of attack of lifting entry vehicles, correlating stagnation point values obtained from heat shield ablation and pressure distribution measurements
Event recorder for in-flight measurements of missile heat-shield ablation
Ablative material degradation in liquid propellant rocket engine environment of nitrogen tetroxide-aerozine
Performance evaluation of low density phenolic nylon, and elastomeric ablative composites
Trajectory optimization and ablation parameters of ballistic models made of eutectic alloys
Ablative and steel chambers effect on combustion instability in hydrogen oxygen rocket engine
Relative erosion resistance of ablative materials for nozzle sections of storable-propellant rocket engine
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