Assessment of high enthalpy flow conditions for re-entry aerothermodynamics in the plasma wind tunnel facilities at IRS
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S. Fasoulas | G. Herdrich | S. Loehle | D. Leiser | F. Zander | M. Eberhart | A. Meindl | T. Hermann | A. Pagan | Fabian Hufgard | B. Massuti-Ballester
[1] M. Friess,et al. Oxidation of PM1000 and C/C-SiC exposed to Highly Dissociated Oxygen and Nitrogen Flows , 2020 .
[2] P. Zell,et al. The Laser Enhanced Arc-Jet Facility (LEAF-Lite): Simulating Convective and Radiative Heating with Arc-jets and Multiple 50-kW CW Lasers , 2018, 2018 Joint Thermophysics and Heat Transfer Conference.
[3] S. Löhle,et al. Fabry–Perot spectroscopy for kinetic temperature and velocity measurements of a high enthalpy air plasma flow , 2017 .
[4] B. Hong,et al. Characteristics of a plasma wind tunnel for the development of thermal protection materials , 2017, The Aeronautical Journal.
[5] F. Colas,et al. Experimental Simulation of Meteorite Ablation during Earth Entry Using a Plasma Wind Tunnel , 2017 .
[6] L. Marraffa,et al. Influence of Ablation on Vacuum-Ultraviolet Radiation in a Plasma Wind Tunnel Flow , 2017 .
[7] G. Herdrich,et al. Experimental Thermal Response and Demisability Investigations on five Aerospace Structure Materials under Simulated Destructive Re-Entry Conditions , 2016 .
[8] S. Loehle. Review of Heat Flux Measurements for High Enthalpy Flows , 2016 .
[9] S. Fasoulas,et al. Characterization of a Reentry Plasma Wind-Tunnel Flow with Vacuum-Ultraviolet to Near-Infrared Spectroscopy , 2016 .
[10] S. Fasoulas,et al. Local Mass-Specific Enthalpy Measurements with a New Mass Injection Probe , 2016 .
[11] M. Fertig,et al. Recent catalysis measurements at IRS , 2015 .
[12] Tahir Gokcen,et al. Consolidating NASA's Arc Jets , 2015 .
[13] Stefanos Fasoulas,et al. Two-Photon Absorption Laser-Induced Fluorescence Investigation of CO2 Plasmas for Mars Entry , 2014 .
[14] Christopher O. Johnston,et al. Characterization of Stagnation-Point Heat Flux for Earth Entry , 2014 .
[15] Robin Beck,et al. Testing of Candidate Rigid Heat Shield Materials at LHMEL for the Entry, Descent, and Landing Technology Development Project , 2012 .
[16] A. Brandis,et al. Numerical Investigation of the Re-entry Flight of Hayabusa and Comparison to Flight Data , 2012 .
[17] H. Roeser,et al. Enhanced Evaluation of Recombination Coefficient Measurements in Plasma Wind Tunnels , 2009 .
[18] D. Petkow,et al. High-enthalpy, water-cooled and thin-walled ICP sources characterization and MHD optimization , 2008, Journal of Plasma Physics.
[19] Raffaele Savino,et al. The GHIBLI plasma wind tunnel: Description of the new CIRA-PWT facility , 2006 .
[20] Michael Winter,et al. The In- Flight Sensor Systems PYREX, PHLUX and RESPECT for the Capsule EXPERT , 2006 .
[21] O. Chazot,et al. Comparative Heat Flux Measurements on Standard Models in Plasma Facilities , 2005 .
[22] M. Auweter-Kurtz,et al. Plasma source development for technical applications at IRS , 2004 .
[23] Paul Zarchan,et al. Advanced Hypersonic Test Facilities , 2002 .
[24] M. Auweter-Kurtz,et al. Mars entry simulation using the inductively heated plasma generator IPG4 , 2001 .
[25] Monika Auweter-Kurtz,et al. Investigation of the inductively heated plasmagenerator IPG3 using injection rings of different geometries , 2000 .
[26] M. Auweter-Kurtz,et al. Estimation of the surface catalycity of PVD-coatings by simultaneous heat flux and LIF measurements in high enthalpy air flows , 2000 .
[27] Monika Auweter-Kurtz,et al. New inductively heated plasma source for reentry simulations , 2000 .
[28] R. Gupta,et al. Aerothermodynamic Analysis of Stardust Sample Return Capsule With Coupled Radiation and Ablation , 1999 .
[29] James Cunningham,et al. A Survey of Current and Future Plasma Arc-Heated Test Facilities for Aerospace and Commercial Applications , 1998 .
[30] Monika Auweter-Kurtz,et al. Plasma generators for re-entry simulation , 1996 .
[31] Monika Auweter-Kurtz,et al. Experimental and theoretical investigation of the oxidation behaviour of thermal protection materials under oxygen attack , 1995 .
[32] S. Fasoulas,et al. The IRS plasma wind tunnels as a tool for the investigation of planet entry missions , 1992 .
[33] M. Auweter-Kurtz,et al. Experimental investigations of MPD devices used as reentry test plasma sources , 1990 .
[34] Monika Auweter-Kurtz,et al. Cathode Erosion Studies on MPD Thrusters , 1985 .
[35] Ronald B. Pope,et al. Laminar convective heating and ablation in the Mars atmosphere. , 1967 .
[36] F. R. Riddell,et al. Theory of Stagnation Point Heat Transfer in Dissociated Air , 1958 .