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Lightweight CFRP frame structures for a ROTEX-derived manipulator system
Reentry flight and ground testing experience with hot structures of C/C-SiC material
A CMC-Based Thermal Protection System for Cryogenic Tank Reusable Launch Vehicles
Behaviour of C/SiC Materials in both Reentry and H2/O2 Combustion Environment
Development of Hot CMC Structures for Space Reentry Vehicles via Flight Experiments
Reentry Flight and Ground Testing Experience with Hot Structures of C/C-SiC Material