Melting ablation about decelerating spherical bodies.
Heat transfer and melting ablation about decelerating spherical bodies during planetary atmosphere entry
PLANETARY ENTRY↗
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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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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↗
Performance of five ablation materials as coating for structures in a region of separated flow
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
SEPARATED FLOW↗
An analysis of a charring ablation thermal protection system
Analytical model for predicting transient one- dimensional thermal performance of charring- ablator heat-protection system exposed to hyperthermal environment
THERMAL PROTECTION↗
Experimental evaluation of various nonmetallic ablative materials as nozzle sections of hydrogen-oxygen rocket engine
Evaluation and erosion of nonmetallic ablating materials as rocket nozzle sections
ROCKET NOZZLE↗
Heat-shield ablation measurements using radioisotope techniques
Radioactive isotope technique for heat shield ablation measurement during reentry
RADIOACTIVE ISOTOPE↗
Investigation of the effect of material properties on composite ablative material behavior Third quarterly report, Dec. 11, 1965 - Mar. 10, 1966
Effects of processing and fabrication techniques on properties of composite ablative materials
ABLATING MATERIAL↗
Experimental evaluation of several ablative materials as nozzle sections of a storable- propellant rocket engine
Ablative material evaluation for nozzle sections of storable propellant rocket engine
ROCKET NOZZLE↗
A calculation method for the ablation of glass-tipped blunt bodies
Trajectory and ablation characteristics calculation for glass-tipped blunt bodies in atmospheric entry
BLUNT BODY↗
Investigation of 3-D fabrication of ablative materials Quarterly progress report no. 1, 8 Sep. - 7 Dec. 1965
Three-dimensional, reinforced fabric construction for ablating materials
ABLATING MATERIAL↗
Study of meteoroid impact into ablative heat shield materials Final report
Meteoroid impact damage to Apollo and Gemini ablative heat shields
GEMINI PROJECT↗
Analytical and experimental study of ablation material for rocket engine application Final report
Techniques for rating performance of ablative materials in liquid-propellant rocket engines
ABLATING MATERIAL↗
Development of Ablation Sensors for Advanced Reentry Vehicles
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal parameters of ablative reentry vehicle heat shield
ABLATING MATERIAL↗
Development and fabrication of ablative optical beacons Final report, 4 Dec. 1965 - 30 Apr. 1966
Lifetime, reliability, and radiation spectrum of ablative flash lamp for Apollo command service module
LIFETIME↗