Determination of effects of oxidation on performance of charring ablators
Effects of oxidation on performance of charring ablating materials
OXIDATION↗
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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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Heat-transfer rates and ablation on a blunted cylinder-flare configuration in free flight up to a mach number of 8.98
Heat-transfer rates and ablation on blunt flared cylinder in free flight at hypersonic and lower speeds
HYPERSONIC SPEED↗
Analysis of the aerodynamic ablation of a metal sphere
Aerodynamic ablation of metal sphere at hypersonic speeds
HYPERSONIC SPEED↗
Hemispherical spectral emittance of ablation chars, carbon, and zirconia to 6,000 deg f.
Optical techniques for high temperature emittance and reflectance studies of ablation material char
SPECTRAL EMISSION↗
Comparison of measurements of internal temperatures in ablation material by various thermocouple configurations
Internal temperatures of ablating material measured by thermocouple configurations
THERMOCOUPLE↗
Hemispherical spectral emittance of ablation chars, carbon, and zirconia to 3700 deg k
Hemispherical spectral emittance of ablation chars, carbon, and zirconia during atmospheric reentry
ABLATION↗
Measurement of optical radiation from the wake of ablating blunt bodies in flight at speeds up to 10 km per second
Optical radiation from wakes of blunt bodies of ablating material measured at hypersonic speeds
LIGHT↗
Analytical study to extend the capabilities of the aerojet-general ablation digital computer program final report
Modified computer program mathematical theory and mathematical model description for predicting rocket engine ablative liner thickness, char depth, and temperature distribution
MATHEMATICAL MODEL↗
Effect of composition and density on the ablative performance of phenolic-nylon
Composition and density effects on ablative performance of phenolic-nylon
PHENOL RESIN↗
Effect on meteor flight of cooling by radiation and ablation
Evaluation of meteor flight parameters taking into account surface radiation and vapor ablation
ABLATION↗
Hemispherical spectral emittance of ablation chars, carbon, and zirconia /to 3700 deg k/
Hemispherical spectral emission of ablation chars, carbon, and zirconium oxide formed during reentry
ZIRCONIUM OXIDE↗
Experimental investigation of a charring ablative material exposed to combined convec- tive and radiative heating in oxidizing and nonoxidizing environments
Interaction between material ablation products and simulated atmosphere entry heat studied in tests on phenolic nylon
ABLATING MATERIAL↗
Melting ablation about decelerating spherical bodies.
Heat transfer and melting ablation about decelerating spherical bodies during planetary atmosphere entry
PLANETARY ENTRY↗
The influence of ablation on stagnation region convective heating for dissociated and partially ionized boundary-layer flows.
Convective heat transfer through high temperature boundary layers with and without ablation products
BOUNDARY LAYER↗
Ablation characteristics and their evaluation by means of arc jets and arc radiation sources.
Ablation process of charring and vaporizing material at stagnation point in entry condition, noting test facilities and principles
ABLATING MATERIAL↗
Determination of parameters necessary for the prediction of ablative heat protection.
Ablative heat protection prediction of material response and environmental factors for ground- based test information
ABLATING MATERIAL↗
The design of ablative thermal protection systems.
Ablative thermal protection system for Apollo command module
THERMAL INSULATION↗
Heat-shield ablation and sublimation determinations through radioisotope techniques.
Heat-shield sublimation and ablation determination during atmospheric reentry, using radioactive technique
ABLATION↗