ABLATING HEAT SHIELDS FOR LOW-ANGLE RE-ENTRY
Reports on the ablation of teflon and polyethylene heat shields for low-angle reentry
POLYETHYLENE↗
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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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NEW RE-ENTRY SHAPES. H
Heat transfer and heating mechanisms in new reentry nose cone shapes
HEAT TRANSFER↗
Approximate analysis of the performance of char-forming ablators
Approximate analysis of performance of charring ablators
ABLATING MATERIAL↗
Synthesis and characterization of model polymers for use in the investigation of char forming heat shields status report no. 1
Model polymer synthesis for use in char forming heat shields
HEAT SHIELD↗
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↗
Thermal balance and heat protection.
Protection of spacecraft against thermal environment during launching, flight and reentry phases, emphasizing charring and melting ablator systems
THERMAL PROTECTION↗
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↗
The effect of injector design on thrust- chamber erosion.
Control of injector spray and heat transfer properties can reduce erosion of ablative and pyrolytic graphite thrust-chamber throats
INJECTOR↗
The design of ablative thermal protection systems.
Ablative thermal protection system for Apollo command module
THERMAL INSULATION↗
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↗
Entry Performance of the Mercury Spacecraft Heat Shield
Flight performance characteristics of Mercury capsule ablative heat shield
HEAT SHIELD↗
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↗
Analytical determination of the effect of thermal property variations on the performance of a charring ablator
Effects of thermal-property variations on performance of charring ablator
ABLATING MATERIAL↗
Exploratory investigation of the effect of nylon grain size on ablation of phenolic nylon
Exploratory investigation of nylon grain size effect on ablation of phenolic nylon
NYLON↗
Design data for ablators. Part III - Mathematical model for decomposition of phenol-formaldehyde ablators Final report
Mathematical model for pyrolytic mechanics of phenol formaldehyde ablators
PYROLYSIS↗
Free-flight aerodynamics of a blunt-faced reentry shape with and without ablation.
Hypersonic aerodynamic stability and drag of ablating and nonablating models of blunt-faced reentry shape
BLUNT BODY↗
Analysis of the effects of environmental conditions on the performance of charring ablators.
Effectiveness of charring ablators strongly influenced by stream enthalpy level and heating rate
REENTRY SHIELD↗