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
Quantitative evaluation of structural damage in lightweight armor materials via XCT
Kinetics and mechanism of oxidation of the reinforced carbon/carbon on the space shuttle orbiter
Grain boundary engineering of silicon carbide by means of coprecipitation
Impact onto glass and glass ceramic bars
Fragmentation of ceramics in the ballistic environment
Ballistic damage assessment of a thin compound curved B4C ceramic plate using XCT