Hermann Hald

发表

Investigations on Fibre Reinforced Combustion Chamber Structures under Effusion Cooled LOX/LH2 Operation

Markus Ortelt, Armin Herbertz, Hermann Hald, 2009 .

Milestones towards hot CMC structures for operational space reentry vehicles

Hermann Hald, H. Weihs, T. Reimer, 2002 .

Potential Applications of the Ceramic Thrust Chamber Technology for Future Rocket Propulsion

Markus Ortelt, Armin Herbertz, Hermann Hald, 2011 .

Advanced Materials for Thrust Chamber Technologies

Hermann Hald, Oskar Haidn, E. Serbest, 2000 .

Porous Injector Concept for a Space Exploration Engine

Markus Ortelt, Armin Herbertz, Hermann Hald, 2010 .

High Temperature Test of a Hinge Joint Attachment of a CMC Control Flap

Hermann Hald, H. Weihs, T. Reimer, 1999 .

Ceramic activities for space propulsion

Markus Ortelt, Armin Herbertz, Hermann Hald, 2012 .

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

Hermann Hald, H. Hald, 2003 .

Potential Applications of the Ceramic Thrust Chamber Technology for Future Transpiration Cooled Rocket Engines

Markus Ortelt, Armin Herbertz, Hermann Hald, 2012 .

Design of a CMC-Based Thermal Protection System for the Cryogenic Tank of a Reusable Space Transportation System.

Hermann Hald, H. Weihs, T. Reimer, 1996 .

Advanced Design Concepts for Ceramic Thrust Chamber Components of Rocket Engines

Markus Ortelt, Armin Herbertz, Hermann Hald, 2013 .

Fluid injection head for combustion chamber, has sections interpenetrating coaxially at axis and having wall zones delimiting distributor channels having extended output zones associated with fuel and oxidation agent flow respectively

Markus Ortelt, Hermann Hald, Oskar Haidn, 2005 .

Structural Investigations on Cryogenically Operated and Transpiration Cooled Fiber Reinforced Rocket Thrust Chambers

Markus Ortelt, Armin Herbertz, Hermann Hald, 2012 .

Development of hot CMC structures for space reentry vehicles via flight experiments

Hermann Hald, Thomas Reimer, Hendrik Weihs, 2003 .

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

Markus Ortelt, Armin Herbertz, Hermann Hald, 2004 .

Effusion Cooled Rocket Combustion Chamber

Markus Ortelt, Hermann Hald, Oskar Haidn, 2005 .

Application of Fiber Reinforced C/C Ceramic Structures in Liquid Rocket Engines

Markus Ortelt, Armin Herbertz, Hermann Hald, 2005 .

Technological Aspects of Transpiration Cooled Composite Structures for Thrust Chamber Applications

Markus Ortelt, Armin Herbertz, Hermann Hald, 2009 .

Development of a CMC-based TPS for two representative specimens of cryogenic tank RLVs

Hermann Hald, H. Weihs, T. Reimer, 1998 .

New Composite Combustion Chambers for Rocket Engines

Markus Ortelt, Hermann Hald, Heinz Voggenreiter, 2008 .

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

Markus Ortelt, Armin Herbertz, Hermann Hald, 2012 .

Current activities in the field of ceramic based rocket engines

Markus Ortelt, Armin Herbertz, Hermann Hald, 2013 .

Technology Status of an Effusion Cooled CMC Rocket Combustion Chamber

Markus Ortelt, Hermann Hald, Ingo Fischer, 2005 .

Empirical Verification of Effusion Cooled CMC Rocket Thrust Chambers

Markus Ortelt, Hermann Hald, Oskar Haidn, 2005 .

$$c^*$$c∗-Efficiency evaluation of transpiration cooled ceramic combustion chambers

Markus Ortelt, Armin Herbertz, Hermann Hald, 2014 .

Reentry Flight Testing of a C/C-SiC Structure with Yttrium Silicate Oxidation Protection

Hermann Hald, Thomas Reimer, Thomas Ullmann, 2006 .

Status and future perspectives of the CMC rocket thrust chamber development at DLR

Markus Ortelt, Hermann Hald, Ilja Müller, 2014 .

Transpiration Cooling of Liquid Rocket Engines Applying Fiber-Reinforced C/C Structures

Markus Ortelt, Armin Herbertz, Hermann Hald, 2003 .

CMC rocket combustion chamber with effusion cooling

Markus Ortelt, Hermann Hald, Dirk Greuel, 2003 .

Development of a CMC nose cap for X-38

Hermann Hald, H. Weihs, T. Reimer, 2001 .

Porous versus porthole fuel injection in a radical farming scramjet: A numerical analysis

Bianca R. Capra, Russell R. Boyce, Hermann Hald, 2015 .

Reentry Flight and Ground Testing Experience with Hot Structures of C/C-SiC Material

Hermann Hald, Thomas Ullmann, T. Ullmann, 2003 .

Application of Transpiration Cooling for Hot Structures

Hermann Hald, Markus Kuhn, M. Kuhn, 2008 .

Effusion Cooling of Throat Region in Rocket Engines Applying Fibre Reinforced Ceramics

Hermann Hald, Oskar Haidn, E. Serbest, 2001 .

Comprehensive C/C sample characterizations for transpiration cooling applications

Hermann Hald, Markus Selzer, Sven Schweikert, 2016 .

Effusion Cooling in Rocket Combustors Applying Fiber Reinforced Ceramics

Hermann Hald, Oskar Haidn, E. Serbest, 1999 .

Development of an attachment system for the CMC nose cap of X-38

Hermann Hald, H. Weihs, T. Reimer, 2001 .

Measurements of surface exhalation characteristics of porous fibre reinforced composites.

Hermann Hald, Markus Selzer, Sven Schweikert, 2012 .

H2-O2 porous fuel injection in a radical farming scramjet

Bianca R. Capra, Russell R. Boyce, Hermann Hald, 2012 .

Experimental Investigations of Transpiration Cooled CMC's in Supersonic Plasma Flows

Herbert Olivier, Hermann Hald, Ali Gülhan, 2006 .

Transfer of an analytical transpiration cooling model to the cooling analysis of rocket combustion chambers made of ceramic matrix composites

Hermann Hald, Markus Selzer, Sven Schweikert, 2013 .

Characterization of Actively Cooled Porous C/C Wall Segments According to Pressure Loss and Internal Temperature Distribution

Hermann Hald, Markus Selzer, Sven Schweikert, 2013 .