HYDRA, A New Hybrid Thermal Protection System for LEO and Moon Mission Re-Entry Vehicles
Manufacturing of the CMC nose CAP for the expert spacecraft
Kinetics and mechanism of oxidation of the reinforced carbon/carbon on the space shuttle orbiter
Quantitative evaluation of structural damage in lightweight armor materials via XCT
Instrumented hertzian indentation study of two commerical silicon carbides
Evaluation of ballistically-induced damage in ceramic targets by X-ray computed tomography
Applying modeling tools to predict performance of transparent ceramic laminate armors