Enhancing TPS Material Characterization for Improved Margin Quantification

This project focuses on improving the reliability of thermal protection systems (TPS) for spacecraft by developing rigorous methods to characterize and certify TPS materials. It aims to reduce uncertainty in material response models by better linking arc-jet test data to predictions; ensuring future spacecraft safety; especially for novel materials like HEEET.

This project will benefit NASA by improving the reliability of thermal protection systems (TPS) through rigorous uncertainty quantification methods. By linking arc-jet test data to TPS material models and incorporating modern stochastic approaches; the project aims to enhance the safety and efficiency of spacecraft design; particularly for novel materials.

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