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Erschienen in: Journal of Materials Science 13/2014

01.07.2014

Material response characterization of a low-density carbon composite ablator in high-enthalpy plasma flows

verfasst von: Bernd Helber, Cem O. Asma, Yacine Babou, Annick Hubin, Olivier Chazot, Thierry E. Magin

Erschienen in: Journal of Materials Science | Ausgabe 13/2014

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Abstract

Future space exploration missions beyond Earth’s orbit, such as sample returns from Mars, will use ablative materials for the thermal protection system in order to shield the spacecraft from the severe heating during reentry. In this paper, we present the results of an elaborate test campaign on a lightweight carbon composite ablator with the aim of defining a procedure for material response characterization in a 1.2-MW inductively heated Plasmatron facility, suitable to reproduce the hypersonic flight boundary layer environment. Three different test gases were used, air, nitrogen, and argon, at surface temperatures exceeding 3300 K. A comprehensive experimental setup was developed including a nonintrusive technique to measure surface recession by means of a high-speed camera. Surface degradation was strongly test gas dependent, while mass loss was mainly driven by in-depth decomposition of phenolic resin. Emission spectroscopy helped us identify C2 as a product of dissociating hydrocarbons, as well as cyanogen, suggesting surface nitridation. Melt flow at the surface and silicon emission indicated degradation of the glass microspheres used as additional filler. In air plasma, oxidation was inferred to be the main mechanism for ablation.

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Literatur
1.
Zurück zum Zitat Altmann I, Bauer G, Hirsch K, Jentschke H, Stefan K, Roth B, Schinköth D, Schumacher U (2000) In-situ diagnostics of the interaction region between a nitrogen–oxygen plasma jet and hot C/C–SiC ceramic materials. High Temp-High Press 32:573–579CrossRef Altmann I, Bauer G, Hirsch K, Jentschke H, Stefan K, Roth B, Schinköth D, Schumacher U (2000) In-situ diagnostics of the interaction region between a nitrogen–oxygen plasma jet and hot C/C–SiC ceramic materials. High Temp-High Press 32:573–579CrossRef
2.
Zurück zum Zitat Asma C, Helber B, Di Lello L, Panerai F, Magin T (2010) Infrared thermography measurements on ablative thermal protection systems for interplanetary space vehicles. In: 10th Quantitative infrared thermography conference, Quebec City, pp 273–277 Asma C, Helber B, Di Lello L, Panerai F, Magin T (2010) Infrared thermography measurements on ablative thermal protection systems for interplanetary space vehicles. In: 10th Quantitative infrared thermography conference, Quebec City, pp 273–277
3.
Zurück zum Zitat Barbante P, Chazot O (2006) Flight extrapolation of plasma wind tunnel stagnation region flowfield. J Thermophys Heat Transfer 20(3):493–499CrossRef Barbante P, Chazot O (2006) Flight extrapolation of plasma wind tunnel stagnation region flowfield. J Thermophys Heat Transfer 20(3):493–499CrossRef
4.
Zurück zum Zitat Barbante P, Degrez G, Sarma G (2002) Computation of nonequilibrium high temperature axisymmetric boundary-layer flows. J Thermophys Heat Transfer 16(4):490–497CrossRef Barbante P, Degrez G, Sarma G (2002) Computation of nonequilibrium high temperature axisymmetric boundary-layer flows. J Thermophys Heat Transfer 16(4):490–497CrossRef
5.
Zurück zum Zitat Bottin B, Chazot O, Carbonaro M, van der Haegen V, Paris S (1999) The VKI plasmatron characteristics and performance. In: RTO AVT course on measurement techniques for high enthalpy and plasma flows, RTO EN-8, Belgium Bottin B, Chazot O, Carbonaro M, van der Haegen V, Paris S (1999) The VKI plasmatron characteristics and performance. In: RTO AVT course on measurement techniques for high enthalpy and plasma flows, RTO EN-8, Belgium
6.
Zurück zum Zitat Bottin B (1999) Aerothermodynamic model of an inductively-coupled plasma wind tunnel. PhD thesis, Université de Liège, von Karman Institute for Fluid Dynamics Bottin B (1999) Aerothermodynamic model of an inductively-coupled plasma wind tunnel. PhD thesis, Université de Liège, von Karman Institute for Fluid Dynamics
7.
Zurück zum Zitat Chazot O, Panerai F, Muylaert JM, Thömel J (2010) Catalysis phenomena determination in plasmatron facility for flight experiment design. In: AIAA 2010–1248, 48th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition, Orlando Chazot O, Panerai F, Muylaert JM, Thömel J (2010) Catalysis phenomena determination in plasmatron facility for flight experiment design. In: AIAA 2010–1248, 48th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition, Orlando
8.
Zurück zum Zitat Crouch RK, Walberg GD (1969) An investigation of ablation behavior of avcoat 5026/39M over a wide range of thermal environments. NASA Tech. Mem., TM X-1778 Crouch RK, Walberg GD (1969) An investigation of ablation behavior of avcoat 5026/39M over a wide range of thermal environments. NASA Tech. Mem., TM X-1778
9.
Zurück zum Zitat Degrez G, Vanden Abeele DP, Barbante PF, Bottin B (2004) Numerical simulation of inductively coupled plasma flows under chemical non-equilibrium. Int J Numer Meth Heat Fluid Flow 14(4):538–558CrossRef Degrez G, Vanden Abeele DP, Barbante PF, Bottin B (2004) Numerical simulation of inductively coupled plasma flows under chemical non-equilibrium. Int J Numer Meth Heat Fluid Flow 14(4):538–558CrossRef
10.
Zurück zum Zitat Duffa G (2013) Ablative thermal protection systems modeling. AIAA Education Series, New York Duffa G (2013) Ablative thermal protection systems modeling. AIAA Education Series, New York
11.
Zurück zum Zitat Dunn M, Kang SW (1973) Theoretical and experimental studies of reentry plasmas. In: Contractor report 2232, NASA Langley Research Center, Hampton, VA, USA, prepared by Cornell Aeronautical Laboratory, Inc., Buffalo, 14221 Dunn M, Kang SW (1973) Theoretical and experimental studies of reentry plasmas. In: Contractor report 2232, NASA Langley Research Center, Hampton, VA, USA, prepared by Cornell Aeronautical Laboratory, Inc., Buffalo, 14221
12.
Zurück zum Zitat Edquist K, Hollis B, Dyakonov A, Laub B, Wright M, Rivellini T, Slimko E, Willcockson W (2007) Mars science laboratory entry capsule aerothermodynamics and thermal protection system. In: Aerospace conference, 2007 IEEE, 1–13 Edquist K, Hollis B, Dyakonov A, Laub B, Wright M, Rivellini T, Slimko E, Willcockson W (2007) Mars science laboratory entry capsule aerothermodynamics and thermal protection system. In: Aerospace conference, 2007 IEEE, 1–13
13.
Zurück zum Zitat Edquist KT, Hollis BR, Johnston CO, Bose D, White TR, Mahzari M (2013) Mars science laboratory heatshield aerothermodynamics: design and reconstruction. In: AIAA 2013–2781, 44th AIAA thermophysics conference, San Diego Edquist KT, Hollis BR, Johnston CO, Bose D, White TR, Mahzari M (2013) Mars science laboratory heatshield aerothermodynamics: design and reconstruction. In: AIAA 2013–2781, 44th AIAA thermophysics conference, San Diego
14.
Zurück zum Zitat Esser B, Gülhan A, Koch U, Keller K, Beversdorff M (2009) Dust Particle Effects on TPS Qualification for Martian Atmosphere. In: ESA SP-659, The 6th european symposium on aerothermodynamics for space vehicles, Versailles Esser B, Gülhan A, Koch U, Keller K, Beversdorff M (2009) Dust Particle Effects on TPS Qualification for Martian Atmosphere. In: ESA SP-659, The 6th european symposium on aerothermodynamics for space vehicles, Versailles
15.
Zurück zum Zitat Gülhan A (1999) Application of pyrometry and IR-thermography to high surface temperature measurements. In: RTO AVT course on measurement techniques for high enthalpy and plasma flows, Belgium, pp 9B-1–9B-24 Gülhan A (1999) Application of pyrometry and IR-thermography to high surface temperature measurements. In: RTO AVT course on measurement techniques for high enthalpy and plasma flows, Belgium, pp 9B-1–9B-24
16.
Zurück zum Zitat Helber B, Panerai F, Chazot O, Magin T, Balat-Pichelin M (2012) The reusability limits of carbon/silicon carbide heat shield materials—part 2: volatilization detection by space-& time-resolved emission spectroscopy. In: RTO-EN-AVT-199, paper 20, von Karman Institute, Rhode-Saint-Genèse, Belgium Helber B, Panerai F, Chazot O, Magin T, Balat-Pichelin M (2012) The reusability limits of carbon/silicon carbide heat shield materials—part 2: volatilization detection by space-& time-resolved emission spectroscopy. In: RTO-EN-AVT-199, paper 20, von Karman Institute, Rhode-Saint-Genèse, Belgium
17.
Zurück zum Zitat Herdrich G, Fertig M, Löhle S (2009) Experimental simulation of high enthalpy planetary entries. Open Plasma Phys J 2:150–164CrossRef Herdrich G, Fertig M, Löhle S (2009) Experimental simulation of high enthalpy planetary entries. Open Plasma Phys J 2:150–164CrossRef
18.
Zurück zum Zitat Hsieh CL, Seader JD (1973) Surface ablation of silica-reinforced composites. AIAA J 11(8):1181–1187CrossRef Hsieh CL, Seader JD (1973) Surface ablation of silica-reinforced composites. AIAA J 11(8):1181–1187CrossRef
19.
Zurück zum Zitat Jentschke H, Hirsch K, Klenge S, Schumacher U (1999) High resolution emission and absorption spectroscopy for erosion product analysis in boundary plasmas. Rev Sci Instrum 70:336–339CrossRef Jentschke H, Hirsch K, Klenge S, Schumacher U (1999) High resolution emission and absorption spectroscopy for erosion product analysis in boundary plasmas. Rev Sci Instrum 70:336–339CrossRef
20.
Zurück zum Zitat Kendall R, Bartlett E, Rindal R, Moyer C (1968) An analysis of the coupled chemically reacting boundary layer and charring ablator: part i. NASA CR 1060, NASA Kendall R, Bartlett E, Rindal R, Moyer C (1968) An analysis of the coupled chemically reacting boundary layer and charring ablator: part i. NASA CR 1060, NASA
21.
Zurück zum Zitat Kolesnikov AF (1993) Conditions of Simulation of Stagnation Point Heat Transfer from a High-enthalpy Flow. Fluid Dyn 28(1):131–137CrossRef Kolesnikov AF (1993) Conditions of Simulation of Stagnation Point Heat Transfer from a High-enthalpy Flow. Fluid Dyn 28(1):131–137CrossRef
22.
Zurück zum Zitat Krassilchikoff HW (2006) Procedures for the determination of the cold copper catalycity. PR 2006-18, von Karman Institute for Fluid Dynamics Krassilchikoff HW (2006) Procedures for the determination of the cold copper catalycity. PR 2006-18, von Karman Institute for Fluid Dynamics
23.
Zurück zum Zitat Kruse T, Roth P (1997) Kinetics of C2 reactions during high-temperature pyrolysis of acetylene. J Phys Chem 101:2138–2146CrossRef Kruse T, Roth P (1997) Kinetics of C2 reactions during high-temperature pyrolysis of acetylene. J Phys Chem 101:2138–2146CrossRef
24.
Zurück zum Zitat Lachaud J, Cozmuta I, Mansour N (2010) Multiscale approach to ablation modeling of phenolic impregnated carbon ablators. J Spacecraft Rock 47(6):910–921CrossRef Lachaud J, Cozmuta I, Mansour N (2010) Multiscale approach to ablation modeling of phenolic impregnated carbon ablators. J Spacecraft Rock 47(6):910–921CrossRef
25.
Zurück zum Zitat Laub B, Venkatapathy E (2003) Thermal protection system technology and facility needs for demanding future planetary missions. In: International workshop on planetary probe atmospheric entry and descent trajectory analysis and science, Lisbon, Portugal, pp 239–247 Laub B, Venkatapathy E (2003) Thermal protection system technology and facility needs for demanding future planetary missions. In: International workshop on planetary probe atmospheric entry and descent trajectory analysis and science, Lisbon, Portugal, pp 239–247
27.
Zurück zum Zitat Marine W, Tokarev V, Gerri M, Sentis M, Fogarassy E (1994) Ablation dynamics of silicon based targets in oxygen and nitrogen atomspheres. Thin Solid Films 214:103–108CrossRef Marine W, Tokarev V, Gerri M, Sentis M, Fogarassy E (1994) Ablation dynamics of silicon based targets in oxygen and nitrogen atomspheres. Thin Solid Films 214:103–108CrossRef
28.
Zurück zum Zitat Marschall J, PejakovicÌ D, Fahrenholtz W, Hilmas G, Panerai F, Chazot O (2012) Temperature jump phenomenon during plasmatron testing of zrb2-sic ultra-high temperature ceramics. J Thermophys Heat Transfer 26:559–572CrossRef Marschall J, PejakovicÌ D, Fahrenholtz W, Hilmas G, Panerai F, Chazot O (2012) Temperature jump phenomenon during plasmatron testing of zrb2-sic ultra-high temperature ceramics. J Thermophys Heat Transfer 26:559–572CrossRef
29.
Zurück zum Zitat Martin A, Boyd I, Cozmuta I, Wright M (2010) Chemistry model for ablating carbon-phenolic material during atmospheric re-entry. In: AIAA 2010–1175, 48th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition, Orlando Martin A, Boyd I, Cozmuta I, Wright M (2010) Chemistry model for ablating carbon-phenolic material during atmospheric re-entry. In: AIAA 2010–1175, 48th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition, Orlando
30.
Zurück zum Zitat (1999-2000) Concise encyclopedia of science and technology, 3rd edn. McGraw Hill, New York (1999-2000) Concise encyclopedia of science and technology, 3rd edn. McGraw Hill, New York
31.
Zurück zum Zitat Milos F, Chen YK (1997) Comprehensive model for multicomponent ablation thermochemistry. AIAA. Reno, NV, pp 0141–1997 Milos F, Chen YK (1997) Comprehensive model for multicomponent ablation thermochemistry. AIAA. Reno, NV, pp 0141–1997
32.
Zurück zum Zitat Milos F, Chen YK (2010) Ablation and thermal response property model validation for phenolic impregnated carbon ablator. J Spacecraft Rock 47(5):786–805CrossRef Milos F, Chen YK (2010) Ablation and thermal response property model validation for phenolic impregnated carbon ablator. J Spacecraft Rock 47(5):786–805CrossRef
33.
Zurück zum Zitat Moyer C, Rindal R (1968) An analysis of the coupled chemically reacting boundary layer and charring ablator: Part ii. NASA CR 1061, NASA Moyer C, Rindal R (1968) An analysis of the coupled chemically reacting boundary layer and charring ablator: Part ii. NASA CR 1061, NASA
34.
Zurück zum Zitat Nawaz A, Driver DM, Terrazas-Salinas I, Sepka S (2013) Surface catalysis and oxidation on stagnation point heat flux measurements in high enthalpy Arc Jets. In: AIAA 2013-3138, 44th AIAA thermophysics conference, San Diego Nawaz A, Driver DM, Terrazas-Salinas I, Sepka S (2013) Surface catalysis and oxidation on stagnation point heat flux measurements in high enthalpy Arc Jets. In: AIAA 2013-3138, 44th AIAA thermophysics conference, San Diego
35.
Zurück zum Zitat Panerai F, Chazot O (2012) Characterization of gas/surface interactions for ceramic matrix composites in high enthalpy, low pressure air flow. Mater Chem Phys 134(2–3):597–607CrossRef Panerai F, Chazot O (2012) Characterization of gas/surface interactions for ceramic matrix composites in high enthalpy, low pressure air flow. Mater Chem Phys 134(2–3):597–607CrossRef
37.
Zurück zum Zitat Panerai F (2012) Aerothermochemistry testing of thermal protection systems. PhD thesis, von Karman Institute for Fluid Dynamics/University of Perugia Panerai F (2012) Aerothermochemistry testing of thermal protection systems. PhD thesis, von Karman Institute for Fluid Dynamics/University of Perugia
38.
Zurück zum Zitat Park C, Bogdanoff D (2006) Shock-tube measurements of nitridation coefficients of solid carbon. J Thermophys Heat Transfer 20(3):487–492CrossRef Park C, Bogdanoff D (2006) Shock-tube measurements of nitridation coefficients of solid carbon. J Thermophys Heat Transfer 20(3):487–492CrossRef
39.
Zurück zum Zitat Park C, Jaffe R, Partridge H (2001) Chemical-kinetic parameters of hyperbolic earth entry. J Thermophys Heat Transfer 15(1):76–90CrossRef Park C, Jaffe R, Partridge H (2001) Chemical-kinetic parameters of hyperbolic earth entry. J Thermophys Heat Transfer 15(1):76–90CrossRef
40.
Zurück zum Zitat Park C (1976) Effects of atomic oxygen on graphite ablation. AIAA J 14(11):1640–1642CrossRef Park C (1976) Effects of atomic oxygen on graphite ablation. AIAA J 14(11):1640–1642CrossRef
41.
Zurück zum Zitat Pearse RWB, Gaydon AG (1963) The identification of molecular spectra, 3rd edn. Chapman & Hall Ltd., New York Pearse RWB, Gaydon AG (1963) The identification of molecular spectra, 3rd edn. Chapman & Hall Ltd., New York
42.
Zurück zum Zitat Rini P, Vanden Abeele D, Degrez G (2005) Closed form for the equations of chemically reacting flows under local thermodynamic equilibrium. Phys Rev E Stat Nonlin Soft Matter Phys 72:011204CrossRef Rini P, Vanden Abeele D, Degrez G (2005) Closed form for the equations of chemically reacting flows under local thermodynamic equilibrium. Phys Rev E Stat Nonlin Soft Matter Phys 72:011204CrossRef
43.
Zurück zum Zitat Ritter H, Bayle O, Mignot Y, Boulier E, Portela P, Bouilly JM, Sharda R (2011) Ongoing European developments on entry heatshields and TPS materials. In: 8th International planetary probe workshop, Portsmouth, Virginia Ritter H, Bayle O, Mignot Y, Boulier E, Portela P, Bouilly JM, Sharda R (2011) Ongoing European developments on entry heatshields and TPS materials. In: 8th International planetary probe workshop, Portsmouth, Virginia
44.
Zurück zum Zitat Sarma G, Vanden Abeele D, Bottin B, Degrez G (1999) Physico-chemical modelling and numerical simulation of an inductive plasmatron. SAMS 34(2):169–187 Sarma G, Vanden Abeele D, Bottin B, Degrez G (1999) Physico-chemical modelling and numerical simulation of an inductive plasmatron. SAMS 34(2):169–187
45.
Zurück zum Zitat Scala S, Gilbert L (1965) Sublimation of graphite at hypersonic speeds. AIAA J 3(9):1635–1644CrossRef Scala S, Gilbert L (1965) Sublimation of graphite at hypersonic speeds. AIAA J 3(9):1635–1644CrossRef
46.
Zurück zum Zitat Schaefer JW, Flood DT, Reese JJ, Kimble JC (1967) Experimental and analytical evaluation of the Apollo thermal protection system under simulated reentry conditions. Part 2: Analysis of results. NASA Tech. Rep., CR 65818 Schaefer JW, Flood DT, Reese JJ, Kimble JC (1967) Experimental and analytical evaluation of the Apollo thermal protection system under simulated reentry conditions. Part 2: Analysis of results. NASA Tech. Rep., CR 65818
47.
Zurück zum Zitat Sepka S, Gasch M, Beck RA, White S (2012) Testing of candidate rigid heatshield materials at LHMEL for the entry, descent, and landing technology development project. Adv Ceram Coat Mater Extrem Environ II 33(3):129–157 Sepka S, Gasch M, Beck RA, White S (2012) Testing of candidate rigid heatshield materials at LHMEL for the entry, descent, and landing technology development project. Adv Ceram Coat Mater Extrem Environ II 33(3):129–157
48.
Zurück zum Zitat Smith DM, Younker T (2005) Comparative ablation testing of carbon phenolic TPS materials in the AEDC-H1 arcjet. In: AIAA 2005-3263, AIAA/CIRA 13th International space planes and hypersonics systems and technologies conference, Capua. doi:10.2514/6.2005-3263 Smith DM, Younker T (2005) Comparative ablation testing of carbon phenolic TPS materials in the AEDC-H1 arcjet. In: AIAA 2005-3263, AIAA/CIRA 13th International space planes and hypersonics systems and technologies conference, Capua. doi:10.​2514/​6.​2005-3263
49.
Zurück zum Zitat Sommer T, Kruse T, Roth P, Hippler H (1997) Perturbation study on the reaction of C2 with N2 in high-temperature C60/Ar + N2 mixtures. J Phys Chem 101:3720–3725CrossRef Sommer T, Kruse T, Roth P, Hippler H (1997) Perturbation study on the reaction of C2 with N2 in high-temperature C60/Ar + N2 mixtures. J Phys Chem 101:3720–3725CrossRef
50.
Zurück zum Zitat Stackpoole M, Sepka S, Cozmuta I (2008) Post-flight evaluation of stardust sample return capsule forebody heatshield material. In: AIAA 2008-1202, 46th AIAA aerospace sciences meeting and exhibit, Reno Stackpoole M, Sepka S, Cozmuta I (2008) Post-flight evaluation of stardust sample return capsule forebody heatshield material. In: AIAA 2008-1202, 46th AIAA aerospace sciences meeting and exhibit, Reno
51.
Zurück zum Zitat Sutton G (1982) The initial development of ablation heat protection: an historical perspective. J Spacecraft Rock 19(1):3–11CrossRef Sutton G (1982) The initial development of ablation heat protection: an historical perspective. J Spacecraft Rock 19(1):3–11CrossRef
52.
Zurück zum Zitat Szalai C, Beck R, Gasch M, Chavez-Garcia J, Splinter S, Gragg J, Brewer A (2011) Thermal protection system aerothermal screening tests in the HYMETS facility. In: 42nd AIAA thermophysics conference, Honolulu, Hawaii, AIAA-2011-3493 Szalai C, Beck R, Gasch M, Chavez-Garcia J, Splinter S, Gragg J, Brewer A (2011) Thermal protection system aerothermal screening tests in the HYMETS facility. In: 42nd AIAA thermophysics conference, Honolulu, Hawaii, AIAA-2011-3493
53.
Zurück zum Zitat Torre L, Kenny J, Maffezzoli A (1998) Degradation behaviour of a composite material for thermal protection systems: part I—experimental characterization. J Mater Sci 33:3137–3143CrossRef Torre L, Kenny J, Maffezzoli A (1998) Degradation behaviour of a composite material for thermal protection systems: part I—experimental characterization. J Mater Sci 33:3137–3143CrossRef
54.
Zurück zum Zitat Torre L, Kenny JM, Boghetich G, Maffezzoli A (2000) Degradation behaviour of a composite material for thermal protection systems: part III char characterization. J Mater Sci 35:4563–4566CrossRef Torre L, Kenny JM, Boghetich G, Maffezzoli A (2000) Degradation behaviour of a composite material for thermal protection systems: part III char characterization. J Mater Sci 35:4563–4566CrossRef
55.
Zurück zum Zitat Tran H, Johnson C, Rasky D, Hui F, Hsu MT, Chen T, Chen YK, Paragas D, Kobayashi L (1997) Phenolic impregnated carbon ablators (PICA) as thermal protection systems for discovery missions. In: NASA, TM 110440 Tran H, Johnson C, Rasky D, Hui F, Hsu MT, Chen T, Chen YK, Paragas D, Kobayashi L (1997) Phenolic impregnated carbon ablators (PICA) as thermal protection systems for discovery missions. In: NASA, TM 110440
56.
Zurück zum Zitat Tran H (1994) Development of lightweight ceramic ablators and arc jet test results. In: NASA TM-108798 Tran H (1994) Development of lightweight ceramic ablators and arc jet test results. In: NASA TM-108798
57.
Zurück zum Zitat Vanden Abeele D, Degrez G (2000) Efficient computational model for inductive plasmas flows. AIAA J 38(2):234–242CrossRef Vanden Abeele D, Degrez G (2000) Efficient computational model for inductive plasmas flows. AIAA J 38(2):234–242CrossRef
58.
Zurück zum Zitat (2000) World book encyclopedia volume 8 G: millennium 2000. World book, incorporated (2000) World book encyclopedia volume 8 G: millennium 2000. World book, incorporated
Metadaten
Titel
Material response characterization of a low-density carbon composite ablator in high-enthalpy plasma flows
verfasst von
Bernd Helber
Cem O. Asma
Yacine Babou
Annick Hubin
Olivier Chazot
Thierry E. Magin
Publikationsdatum
01.07.2014
Verlag
Springer US
Erschienen in
Journal of Materials Science / Ausgabe 13/2014
Print ISSN: 0022-2461
Elektronische ISSN: 1573-4803
DOI
https://doi.org/10.1007/s10853-014-8153-z

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