Ablative response of a silica phenolic to simulated liquid propellant rocket engine operating conditions
Ablative response of silica phenolic to simulated liquid propellant rocket engine operating conditions
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Ablative response of silica phenolic to simulated liquid propellant rocket engine operating conditions
Computer program for analyzing transient response of ablating axisymmetric bodies including effects of shape change
Analysis of reacting flow of pyrolysis products through char layer of low density, nylon phenolic resin, charring ablators and porous graphite
Ablative heat shield char layer, examining reacting nonequilibrium pyrolysis gas flow
Ablative materials performance in high radiative heat flux environments produced by CW carbon dioxide laser
Thoria dispersed Ni-Cr alloy hypersonic entry ablation model, accounting for Cr oxidation
Artificial meteors ablation and luminosity measurements, using ballistic range shadowgraph and radiometric equipment for velocity history, shock wave formation and mass loss process
Cone roll dynamics-ablation patterns coupling in hypersonic wind tunnels
Epoxy novolac resin-cured alicyclic anhydride amine-catalyzed ablative polymers molecular structure from computer correlation of analytical data
Ablative polymers synthesis from formaldehyde, phenols and ethers reaction products, discussing char yield, thermally stable fillers incorporation and thermogravimetric analysis
Graphite ablation under high temperatures for large outer planets entry probes, correlating mass loss rates with surface temperatures and specimen nose cone radii
Performance prediction of fixed wing leading edges radiative, ablative and active cooling thermal protection systems and system weights comparison for space shuttle entry mission
Nonequilibrium modeling of pyrolysis gas products flow through char layer of ablative heat shield
Large meteoroids ablation and breakup mathematical model, estimating Mars atmosphere effectiveness as shield against surface impact craters production
NASA-SRI Round Robin Ablation Program summary, discussing dimensional analysis, Teflon, nylon and surface temperature
Jupiter atmosphere entry probes graphite ablative heat shields performance, indicating convective and radiative blockage and graphite sublimation processes in surface heat balance
Reflecting and ablating Teflon heat shields for radiative environment of outer planets atmosphere
Development of ablative materials based on modification of polyphenylene compounds is discussed. Chemical and physical properties are analyzed for application as heat resistant materials. Synthesis of linear polyphenylenes is described. Effects of exposure to oxyacetylene flame and composition of resultant char layer are presented.