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Capabilities of RF-plasmatron IPG-4 for re-entry simulation

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The capabilities of the 100-kW IPG-4 plasmatron in terms of the optimal test conditions for simulation of the re-entry stagnation heating of the Pre-X and EXPERT vehicles are presented. Test requirements for the peak-heating parts of the Pre-X and EXPERT trajectories have motivated the different technical approaches to expand the IPG-4 capabilities at the low and high pressure borders of the operating envelope. The simulation of the stagnation point heat transfer is achieved for both re-entry vehicles close to re-entry conditions in terms of the total enthalpy, stagnation pressure and velocity gradient. Catalytic efficiency of SiC surface with respect to surface recombination of oxygen and nitrogen atoms is predicted close to the EXPERT re-entry conditions.
Rocznik
Strony
181--198
Opis fizyczny
Bibliogr. 17 poz., rys., wykr.
Twórcy
  • Institute for Problems in Mechanics, Russian Academy of Sciences, Moscow
Bibliografia
  • 1. A. KOLESNIKOV, The Aerothermodynamic Simulation in Sub- and Supersonic High-Enthalpy Jets: Experiment and Theory, Proc. 2nd European Symposium on Aerothermodynamics for Space Vehicles, ESA SP-367, 583-590, 1995.
  • 2. A. F. KOLESNIKOV, I. S. PERSHIN, S. A. VASIL’EVSKII, VI. I. YAKUSHIN, Study of Quartz Surface Catalycity in Dissociated Carbon Dioxide Subsonic Flows, J. Spacecraft and Rockets, 37, 5, 573-579, 2000.
  • 3. S. A. VASIL'EVSKII, A. F. KOLESNIKOV, M. I. YAKUSHIN, Mathematical Models for Plasma and Gas Flows in Induction Plasmatrons, Molecular Physics and Hypersonic Flows, M. Capitelli [Ed.]. NATO ASI Series, Kluwer, 482, 495-504, 1996.
  • 4. A. Kolesnikov, I.S. Pershin, S.A. Vasil’evskii. Predicting Catalycity of Si-Based Coating and Stagnation Point Heat Transfer in High-Enthalpy CO2 Subsonic Flows for the Mars Entry Conditions. Proc. Int. Workshop ‘Planetary Probe Atmospheric Entry and Descent Trajectory Analysis and Science’, A. Wilson [Ed.], ESA Publication Division, ESA SP-544, 77-83, 2004.
  • 5. A. KOLESNIKOV, A. GORDEEV, S. VASIL’EVSKII, J. L. VERANT, Technical Approach and validation of Reentry Heating Simulation for the Pre-X and EXPERT Vehicles Using the IPG-4 Plasmatron, Proc. EUCASS (CD-ROM), Moscow, Russia 2005.
  • 6. A. KOLESNIKOV, A. GORDEEV, S. VASIL’EVSKII, J.L. VERANT, Predicting Catalytic Properties of SiC Material for the Pre-X Vehicle Re-Entry Conditions, Proc. 2nd EUCASS European Conference for Aero-Space Sciences (CD-ROM), Brussels, Belgium 2007.
  • 7. A. KOLESNIKOV, Conditions of Simulation of Stagnation Point Heat Transfer from a, High-Enthalpy Flow Fluid Dynamics, Plenum (tr. from Russian), 28, 131-137, 1993.
  • 8. A. F. KOLESNIKOV, Extrapolation from High Enthalpy Tests to Flight Based on the Concept of the Local Heat Transfer Simulation, Measurement Techniques for High Enthalpy and Plasma Flows, RTO-EN-8. 8B-1-8B-14, 2000.
  • 9. J. A. FAY, F. R. RIDDELL, Theory of Stagnation Point Heat Transfer in Dissociated Air, J. Aeronaut. Sci., 25, 73-85, 1958.
  • 10. A. F. KOLESNIKOV, V. S. SHCHELIN, Numerical Analysis of Simulation Accuracy for Hypersonic Heat Transfer in Subsonic Jets of Dissociated Nitrogen, Fluid Dynamics, Plenum (tr. From Russian), 25, 2, 278-286, 1990.
  • 11. A. KOLESNIKOV, L. MARRAFFA, An Analysis of Stagnation Point Thermochemical Simulation by Plasmatron for Mars Probe, AIAA Paper 99-3564, 1999.
  • 12. A. F. KOLESNIKOV, The Concept of Local Simulation for Stagnation Point Heat Transfer in Hypersonic Flows: Applications and Validation, AIAA Paper 2000-2515, 2000.
  • 13. V. V. LUNEV, Hypersonic Aerodynamics [in Russian], Mashino-stroenie, Moscow 1975.
  • 14. Surface Catalysis Determination for Earth and Mars Atmospheres Re-entry Vehicles: Microscopic vs Macroscopic Methods, INTAS/CNES PROJECT 5117, July 2004 - July 2006, Year 1 Activities Technical Report, 2005.
  • 15. J. MUYLAERT, M. CAPORICCI, Preparing for Reentry with EXPERT: The ESA in Flight ATD Research Programme, Proc. EUCASS (CD-ROM), Moscow, Russia 2005.
  • 16. S. A. VASIL’EVSKII, A. F. KOLESNIKOV, Numerical simulation of equilibrium induction plasma flows in cylindrical plasmatron channel, Fluid Dynamics, Plenum (tr. from Russian), 35, 769-777, 2000.
  • 17. S. V. PATANKAR, D. B. SPALDING, Heat and Mass Transfer in Boundary Layers, Intertext Books, London 1970.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT5-0060-0003
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