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Hermann Hald

Observed names: Hald, Hermann, Hermann HALD, Ing Hermann Hald
OpenAlex ID: A5113572089
Operational limits for reusable space transportation systems due to physical boundaries of C/SiC materials
2003 · Hermann Hald · Aerospace Science and Technology · 89
Transpiration Cooling Appllied to C/C Liners of Cryogenic Liquid Rocket Engines
2004 · Oskar Haidn, Dirk Greuel, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 46
Technological Aspects of Transpiration Cooled Composite Structures for Thrust Chamber Applications
2009 · Hermann Hald, Armin Herbertz, et al. · AIAA International Space Planes and Hypersonic Systems and Technologies Conference · 28
Effusion Cooled CMC Rocket Combustion Chamber
2005 · Hermann Hald, Markus Ortelt, et al. · AIAA International Space Planes and Hypersonic Systems and Technologies Conference · 27
Transpiration Cooled Ceramic Thrust Chamber Applicability for High-Thrust Rocket Engines
2012 · Armin Herbertz, Markus Ortelt, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC) · 25
Porous Versus Porthole Fuel Injection in a Radical Farming Scramjet: Numerical Analysis
2015 · Bianca R. Capra, Russell R. Boyce, et al. · Journal of Propulsion and Power · 20
Investigations on Fibre Reinforced Combustion Chamber Structures under Effusion Cooled LOX/LH2 Operation
2009 · Markus Ortelt, Hermann Hald, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC) · 15
Reentry Flight and Ground Testing Experience with Hot Structures of C/C-SiC Material
2003 · Hermann Hald, Thomas Ullmann · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 15
Liquid Infiltrated C/SiC : An Alternative Material for Hot Space Structures
1989 · Hermann Hald, Walter Krenkel · 13
Manufacturing of the CMC Nose Cap for the Expert Spacecraft
2010 · Christian Zuber, Thomas Reimer, et al. · Ceramic engineering and science proceedings · 12
$$c^*$$ c ∗ -Efficiency evaluation of transpiration cooled ceramic combustion chambers
2014 · Armin Herbertz, Markus Ortelt, et al. · CEAS Space Journal · 11
Structural Investigations on Cryogenically Operated and Transpiration Cooled Fiber Reinforced Rocket Thrust Chambers
2012 · Markus Ortelt, H. Elsaesser, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC) · 11
Advanced Design Concepts for Ceramic Thrust Chamber Components of Rocket Engines
2013 · Markus Ortelt, Hermann Hald, et al. · elib (German Aerospace Center) · 10
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Novel Hybrid Ablative/Ceramic Development for Re-Entry in Planetary Atmospheric Thermal Protection: Interfacial Adhesive Selection and Test Verification Plan
2014 · Jorge Barcena, Sonia Florez, et al. · AIAA International Space Planes and Hypersonic Systems and Technologies Conference · 9
Experimental Investigations of Transpiration Cooled CMC's in Supersonic Plasma Flows
2006 · Markus Kuhn, Hermann Hald, et al. · elib (German Aerospace Center) · 9
Development of Hot CMC Structures for Space Reentry Vehicles via Flight Experiments
2003 · Hermann Hald, Hendrik Weihs, et al. · AIAA International Air and Space Symposium and Exposition: The Next 100 Years · 9
Production and Characterization of Porous C/C Material
2009 · Markus Selzer, Tobias Langener, et al. · elib (German Aerospace Center) · 8
Potential Applications of the Ceramic Thrust Chamber Technology for Future Transpiration Cooled Rocket Engines
2012 · Armin HERBERTZ, Markus ORTELT, et al. · TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN · 7
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Reentry Flight Testing of a C/C-SiC Structure with Yttrium Silicate Oxidation Protection
2006 · Thomas Ullmann, Thomas Reimer, et al. · AIAA International Space Planes and Hypersonic Systems and Technologies Conference · 7
A porous flow control element for pulsed plasma thrusters
2011 · Hannah Böhrk, Matthias Lau, et al. · CEAS Space Journal · 6
CMC Rocket Combustion Chamber with Effusion Cooling
2003 · Hermann Hald · International Astronautical Congress (IAC) · 6
Status and future perspectives of the CMC rocket thrust chamber development at DLR
2014 · Markus Ortelt, Hermann Hald, et al. · elib (German Aerospace Center) · 5
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Current activities in the field of ceramic based rocket engines
2013 · Markus Ortelt, Fabian Breede, et al. · elib (German Aerospace Center) · 5
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Characterization of Actively Cooled Porous C/C Wall Segments According to Pressure Loss and Internal Temperature Distribution
2013 · Sven Schweikert, Jens von Wolfersdorf, et al. · elib (German Aerospace Center) · 5
Comprehensive C/C sample characterizations for transpiration cooling applications
2016 · Markus Selzer, Sven Schweikert, et al. · elib (German Aerospace Center) · 3
Works count: 56
Citation count: 419
H-index: 11
I10-index: 13
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