SP-629 November 2006 The 2 nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry 6–8 September 2006 University ‘La Sapienza’ Rome, Italy Organised by European Space Agency (ESA) Centre National d’Etudes Spatiales (CNES)
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Radiation of High Temperature Gases in Atmospheric Entry · A Solution for Test-Case 5: Simulation of the Radiative Emission of a Chemical Equilibrium 97% CO2–3% N2 Atmospheric
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SP-629November 2006
The 2nd International Workshop on
Radiation of High TemperatureGases in Atmospheric Entry
Publication Proceedings of the 2nd International Workshop on Radiation ofHigh Temperature Gases in Atmospheric Entry’,University ‘La Sapienza’, Rome, Italy(ESA SP-629, November 2006)
Edited by A. WilsonESA Publications Division
Published and distributed by ESA Publications DivisionESTEC, Noordwijk, The Netherlands
Price EUR 30
ISBN 92-9092-940-5ISSN 1609-042X
Copyright 2006 European Space Agency
CONTENTS
General Interest 1
Chair: F. Mazoué
Structure and Instability of Interacting Flows in Shells Around Evolved StarsJ.-P. Lafon, Observatoire de Paris, France; A.V. Myasnikov, Schlumberger Research andDevelopment, Russia
Conceptual Design of Super-Orbital Earth Entry Flight Experiment using a Submarine-LaunchedVehicleJ.-J. Na et al., Korea advanced Institute of Science and Technology, Korea
Modeling the Spectral Radiation of a Methane /Nitrogen Plasma; Test Case 4L. Caillaut et al., EM2C, France
TC-5 Session
Chairs: M.Y. Perrin & J.H. Grinstead
A Solution for Test-Case 5: Simulation of the Radiative Emission of a Chemical Equilibrium 97%CO2–3% N2 Atmospheric Pressure Plasma PlumeM.L. Da Silva, IST, Portugal; et al.
Palumbo Session
Chairs: M.L. Da Silva & D. Fletcher
Ames Electric Arc Shock Tube (East): Optical Instrumentation and Facility CapabilitiesJ.H. Grinstead, NASA Ames Research Center, USA; et al.
Prediction of Nozzle Throat Condition for Palumbo et al.’s ExperimentJ.-I. Lee, Seoul National University, Korea
Calculation of Nozzle Throat Condition in an Arc-Jet FacilityT. Sakai, Nagoya University, Japan; T. Suzuki, JAXA, Japan
Rebuilding of the Palumbo Experiments in an Arc JetF. Mazoue, AOES, The Netherlands; B. Chassaigne & L. Marraffa, ESA/ESTEC, The Netherlands
Code Development Session
Chairs: S. Surzhikov & A. Soufiani
ESA PlasmA RAdiation DatabasE (PARADE). Development History, Status, CurrentDevelopments and Future ProspectsJ. Dubois & A.J. Smith, FGE, UK
Extension of PARADE to CO2 Plasmas and Comparison with Experimental Data in High SpectralResolution for Air and CO2 SpeciesM.W. Winter et al., IRS, Germany
ERIM Experimental Data Interpretation with the Use of the Hybrid Monte-Carlo/Random ModelS. Surzhikov, IPMech RAS, Russia
TC-2 Session
Chairs: A. Chikhaoui & M. Capitelli
Non-Equilibrium Vibration-Dissociation Kinetics and Heat Transfer in CO2/N2 MixturesE.V. Kustova , Saint Petersburg State University, Russia; et al.
Test Case 2: Monodimensional Radiative Flowfield Simulation in Titan-like AtmosphereY. Ogino et al., Tohoku University, Japan
TC-6 Session
Chairs: A. Smith & P. Reynier
Determination of the Radiation Emission during the Fire II EntryF. Mazoué, AOES, The Netherlands; L. Marraffa, ESA/ESTEC, The Netherlands
Numerical Simulation of Radiative Heating Environment on Test Case 6H. Osawa et al., Tohoku University, Japan
Analysis of Different Kinetic Models of High Temperature Air for Interpretation of the FIRE-IIExperimental DataS. Surzhikov, IPMech RAS, Russia
Radiative Transfer in Earth Re-entry: Application to the Project Fire II ExperimentsJ.-M. Lamet, EM2C, France; et al.
Numerical Investigation Session 1
Chairs: P. Boubert & T. Sakai
State-to-State Chemical Kinetics and Radiation Transport in Nitrogen Atomic Plasma forAerospace ApplicationsG. D’Ammando, Dept. of Chemistry University of Bari, Italy; et al.
TC-3 Session
Chairs: P. Omaly & E. Kustova
Numerical Prediction of Convective and Radiative Heating of a Mars Sampler Return OrbiterN. Bédon et al., IUSTI, France
Convective and Radiative Heating of MSRO, Predicted by Different Kinetic ModelsS. Surzhikov, IPMech RAS, Russia
Prediction of Radiative Flux Distribution over the Front Shield of a Vehicle Entering MartianAtmosphere – Contribution to Test Case TC3Y. Babou et al., EM2C, France
ONERA-CNES Activities on TC3 Test Case IIIO. Rouzaud, ONERA, France; P. Omaly, CNES, France
Numerical Prediction for Mars Atmosphere Entry Vehicle using a Density Based SolverD. Vinteler et al., ESI, France
General Interest 2
Chairs: T. McIntyre & U. Koch
Research Activities around JAXA/ISAS and Japanese Universities, Related to ReentryTechnologiesT. Abe, JAXA, Japan
Numerical Investigation Session 2
Chairs: T. Abe & M. Onofri
Radiation Behind the Strong Shock Wave in CO:N2 MixtureE.M. Anohin et al., Moscow Institute of Physics and Technology, Russia
Determination of Radiation during Mars Entry Flight using a Shock TubeE.-S. Lee, Korea Advanced Institute of Science and Technology, Korea
Numerical Simulations of the Martian Atmosphere in the SCIROCCO Wind TunnelD. Paterna, Dept. of Space Science and Engineering, Italy; et al.
Test Facilities 1
Chairs: L. Marraffa & D. Giordano
Modelling of a DC Arc Plasma Source for the Simulation of Mars Atmosphere around a SpacecraftB. Lopez, LOA, France; et al.
Spectroscopic Investigation of Mars Atmosphere PhotochemistryD. Fletcher et al., VKI, Belgium
Test Facilities 2
Chairs: M. Fertig & M. Dudeck
Raman Scattering Measurements of N2 and O2 in a Flat Plate Boundary Layer of an Air PlasmaD. Studer, CORIA, France; et al.
Impulse Facility Simulation of Hypervelocity Radiating FlowsR. Morgan, University of Queensland, Australia; et al.
Poster Papers
Emission Spectroscopy Activities in CIRAF. De Filippis, CIRA, Italy; et al.
Mars Chemical Kinetic Models: A Short ReviewI. Ndindabahizi, ESA/ESTEC, The Netherlands; et al.
Modelling of Re-entry Flows: Expertise Available at ISAP. Reynier, ISA, France