Physical Challenges and Limitations Confronting the Use of UHTCs on Hypersonic Vehicles
Testing of DLR C/C-SiC and C/C for HIFiRE 8 Scramjet Combustor (AIAA 2014-3089)
Development and Capabilities of the NASA Langley Cryogenic Pressure Box
Development and Capabilities of the NASA Langley Cryogenic Pressure Box
Advanced CMC TPS Design Concepts for Re-usable Re-entry Vehicles