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Analysis and Optimization of Selected Thermostructural
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ablative heat shield ablator materials ablator strain ablator thickness adhesive bond aluminum analysis aspect ratio Autoclave bead stiffened Beryllium configuration cost critical crown panel defined density double skin corrugation Effect of Variation elastomer elevon Figure flutter foil glass heat shield design heat shield panel Heat Shield Temperatures heat shield weight heating rate ratio honeycomb panel Imidite insulation thickness joint material LDNP ablator LDNP system leading edge panel load Martin Company maximum NASA 602 ablator NASA 602 system Nominal re-entry Optimum Weight Curves orbital cold soak overshoot re-entry panel depth Panel Optimum Weight panel support panel weight phenolic phenolic/glass laminate Phenyl-silane plastic laminate pressure room temperature shield design curves single skin corrugation skin corrugation panel stagnation point stainless steel structural efficiency substrate materials SUBSTRATE PANEL DESIGN SUBSTRATE PANEL MATERIALS support spacing Table thermal conductivity thermal stress thermostructural panel concepts Titanium Undershoot re-entry vehicle structure