AN INVESTIGATION OF THE EFFECT OF GAS COMPOSITION ON THE ABLATION BEHAVIOR OF A CHARRING MATERIAL
Chemical interaction between an ablation system, a charring material and high-velocity streams of arc-heated air, nitrogen, and argon
HEAT TRANSFER↗
SEARCH · Search NASA
Results for “ABLATION”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
FREE-FLIGHT INVESTIGATIONS OF SUBLIMING ABLATORS AND TRANSPIRATION COOLING AT HYPERSONIC VELOCITIES
Free flight investigations with solid fuel rocket propelled vehicle systems where the thermal protection was provided by either a subliming ablator or by transpiration cooling
TRANSPIRATION COOLING↗
Analytical Evaluation of Rocket Nozzle Ablation
Method for calculating rates of material ablation in rocket nozzles
ROCKET NOZZLE↗
Photometry, dimensions, and ablation rate of comets
Photometry, dimensions, and ablation rate of comets
ASTRONOMICAL PHOTOMETRY↗
Effect of Gas Composition on the Ablation Behavior of a Charring Material
Ablation behavior of charring material in high velocity streams of arc heated air, nitrogen, and argon
GAS STREAM↗
Approximate analysis of the performance of char-forming ablators
Approximate analysis of performance of charring ablators
ABLATING MATERIAL↗
Determination of effects of oxidation on performance of charring ablators
Effects of oxidation on performance of charring ablating materials
OXIDATION↗
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↗