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
Microstructural examination and quasi-static property determination of sintered armor grade SiC
Grain boundary engineering of silicon carbide by means of coprecipitation
Impact onto glass and glass ceramic bars
Fragmentation of ceramics in the ballistic environment
Defect free spinel ceramics of high strength and high transparency