Hermann Hald

Operational limits for reusable space transportation systems due to physical boundaries of C/SiC materials

Hermann Hald · Aerospace Science and Technology · 2003 · 86 citations

Space Transportation, Engineering, Space Vehicles +8

Transpiration Cooling Appllied to C/C Liners of Cryogenic Liquid Rocket Engines

Oskar Haidn, Dirk Greuel, Armin Herbertz et al. · 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 2004 · 40 citations

Engineering, Liquid Metal Cooling, Mechanical Engineering +19

Technological Aspects of Transpiration Cooled Composite Structures for Thrust Chamber Applications

Hermann Hald, Armin Herbertz, Markus Kuhn et al. · 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference · 2009 · 25 citations

Engineering, Mechanical Engineering, Thermoplastic Composite +18

Effusion Cooled CMC Rocket Combustion Chamber

Hermann Hald, Markus Ortelt, Ingo Fischer et al. · AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference · 2005 · 25 citations

Engineering, Combustion Science, Mechanical Engineering +6

Transpiration Cooled Ceramic Thrust Chamber Applicability for High-Thrust Rocket Engines

Armin Herbertz, Markus Ortelt, Ilja Müller et al. · 2012 · 21 citations