A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility
The following work reports a study that uses spontaneous emission spectroscopy for the evaluation of the average temperatures of the plasma shock layer and the test article surfaces subject to the hypersonic jet generated by the Plasma Wind Tunnel (PWT) facility at CIRA. Besides the qualitative info...
Ausführliche Beschreibung
Autor*in: |
Savino, L. [verfasserIn] Martucci, A. [verfasserIn] Del Vecchio, A. [verfasserIn] De Cesare, M. [verfasserIn] |
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Format: |
E-Artikel |
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Sprache: |
Englisch |
Erschienen: |
2020 |
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Schlagwörter: |
Plasma and surface temperature in hypersonic conditions Materials emissivity at hypersonic speeds Near infrared and long wavelength surface emissivity |
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Übergeordnetes Werk: |
Enthalten in: Infrared physics & technology - Amsterdam [u.a.] : Elsevier Science, 1994, 108 |
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Übergeordnetes Werk: |
volume:108 |
DOI / URN: |
10.1016/j.infrared.2020.103353 |
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Katalog-ID: |
ELV004229606 |
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245 | 1 | 0 | |a A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility |
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520 | |a The following work reports a study that uses spontaneous emission spectroscopy for the evaluation of the average temperatures of the plasma shock layer and the test article surfaces subject to the hypersonic jet generated by the Plasma Wind Tunnel (PWT) facility at CIRA. Besides the qualitative information about the species of the hypersonic free stream emission generated by the SCIROCCO arcjet plasma tunnel, the most powerful PWT in the world, the main emission from the species in the shock layer can be obtained. | ||
650 | 4 | |a Optical emission spectroscopy | |
650 | 4 | |a Plasma and surface temperature in hypersonic conditions | |
650 | 4 | |a Materials emissivity at hypersonic speeds | |
650 | 4 | |a Near infrared and long wavelength surface emissivity | |
650 | 4 | |a Planck law distribution | |
650 | 4 | |a Black body calibration spectrum | |
650 | 4 | |a Spectrometric and thermographic data | |
700 | 1 | |a Martucci, A. |e verfasserin |4 aut | |
700 | 1 | |a Del Vecchio, A. |e verfasserin |4 aut | |
700 | 1 | |a De Cesare, M. |e verfasserin |4 aut | |
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2020 |
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10.1016/j.infrared.2020.103353 doi (DE-627)ELV004229606 (ELSEVIER)S1350-4495(20)30401-1 DE-627 ger DE-627 rda eng 530 DE-600 50.37 bkl 33.38 bkl 33.07 bkl Savino, L. verfasserin aut A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility 2020 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The following work reports a study that uses spontaneous emission spectroscopy for the evaluation of the average temperatures of the plasma shock layer and the test article surfaces subject to the hypersonic jet generated by the Plasma Wind Tunnel (PWT) facility at CIRA. Besides the qualitative information about the species of the hypersonic free stream emission generated by the SCIROCCO arcjet plasma tunnel, the most powerful PWT in the world, the main emission from the species in the shock layer can be obtained. Optical emission spectroscopy Plasma and surface temperature in hypersonic conditions Materials emissivity at hypersonic speeds Near infrared and long wavelength surface emissivity Planck law distribution Black body calibration spectrum Spectrometric and thermographic data Martucci, A. verfasserin aut Del Vecchio, A. verfasserin aut De Cesare, M. verfasserin aut Enthalten in Infrared physics & technology Amsterdam [u.a.] : Elsevier Science, 1994 108 Online-Ressource (DE-627)320592146 (DE-600)2019084-0 (DE-576)259271705 nnns volume:108 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.37 Technische Optik 33.38 Quantenoptik nichtlineare Optik 33.07 Spektroskopie AR 108 |
spelling |
10.1016/j.infrared.2020.103353 doi (DE-627)ELV004229606 (ELSEVIER)S1350-4495(20)30401-1 DE-627 ger DE-627 rda eng 530 DE-600 50.37 bkl 33.38 bkl 33.07 bkl Savino, L. verfasserin aut A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility 2020 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The following work reports a study that uses spontaneous emission spectroscopy for the evaluation of the average temperatures of the plasma shock layer and the test article surfaces subject to the hypersonic jet generated by the Plasma Wind Tunnel (PWT) facility at CIRA. Besides the qualitative information about the species of the hypersonic free stream emission generated by the SCIROCCO arcjet plasma tunnel, the most powerful PWT in the world, the main emission from the species in the shock layer can be obtained. Optical emission spectroscopy Plasma and surface temperature in hypersonic conditions Materials emissivity at hypersonic speeds Near infrared and long wavelength surface emissivity Planck law distribution Black body calibration spectrum Spectrometric and thermographic data Martucci, A. verfasserin aut Del Vecchio, A. verfasserin aut De Cesare, M. verfasserin aut Enthalten in Infrared physics & technology Amsterdam [u.a.] : Elsevier Science, 1994 108 Online-Ressource (DE-627)320592146 (DE-600)2019084-0 (DE-576)259271705 nnns volume:108 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.37 Technische Optik 33.38 Quantenoptik nichtlineare Optik 33.07 Spektroskopie AR 108 |
allfields_unstemmed |
10.1016/j.infrared.2020.103353 doi (DE-627)ELV004229606 (ELSEVIER)S1350-4495(20)30401-1 DE-627 ger DE-627 rda eng 530 DE-600 50.37 bkl 33.38 bkl 33.07 bkl Savino, L. verfasserin aut A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility 2020 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The following work reports a study that uses spontaneous emission spectroscopy for the evaluation of the average temperatures of the plasma shock layer and the test article surfaces subject to the hypersonic jet generated by the Plasma Wind Tunnel (PWT) facility at CIRA. Besides the qualitative information about the species of the hypersonic free stream emission generated by the SCIROCCO arcjet plasma tunnel, the most powerful PWT in the world, the main emission from the species in the shock layer can be obtained. Optical emission spectroscopy Plasma and surface temperature in hypersonic conditions Materials emissivity at hypersonic speeds Near infrared and long wavelength surface emissivity Planck law distribution Black body calibration spectrum Spectrometric and thermographic data Martucci, A. verfasserin aut Del Vecchio, A. verfasserin aut De Cesare, M. verfasserin aut Enthalten in Infrared physics & technology Amsterdam [u.a.] : Elsevier Science, 1994 108 Online-Ressource (DE-627)320592146 (DE-600)2019084-0 (DE-576)259271705 nnns volume:108 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.37 Technische Optik 33.38 Quantenoptik nichtlineare Optik 33.07 Spektroskopie AR 108 |
allfieldsGer |
10.1016/j.infrared.2020.103353 doi (DE-627)ELV004229606 (ELSEVIER)S1350-4495(20)30401-1 DE-627 ger DE-627 rda eng 530 DE-600 50.37 bkl 33.38 bkl 33.07 bkl Savino, L. verfasserin aut A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility 2020 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The following work reports a study that uses spontaneous emission spectroscopy for the evaluation of the average temperatures of the plasma shock layer and the test article surfaces subject to the hypersonic jet generated by the Plasma Wind Tunnel (PWT) facility at CIRA. Besides the qualitative information about the species of the hypersonic free stream emission generated by the SCIROCCO arcjet plasma tunnel, the most powerful PWT in the world, the main emission from the species in the shock layer can be obtained. Optical emission spectroscopy Plasma and surface temperature in hypersonic conditions Materials emissivity at hypersonic speeds Near infrared and long wavelength surface emissivity Planck law distribution Black body calibration spectrum Spectrometric and thermographic data Martucci, A. verfasserin aut Del Vecchio, A. verfasserin aut De Cesare, M. verfasserin aut Enthalten in Infrared physics & technology Amsterdam [u.a.] : Elsevier Science, 1994 108 Online-Ressource (DE-627)320592146 (DE-600)2019084-0 (DE-576)259271705 nnns volume:108 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.37 Technische Optik 33.38 Quantenoptik nichtlineare Optik 33.07 Spektroskopie AR 108 |
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530 DE-600 50.37 bkl 33.38 bkl 33.07 bkl A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility Optical emission spectroscopy Plasma and surface temperature in hypersonic conditions Materials emissivity at hypersonic speeds Near infrared and long wavelength surface emissivity Planck law distribution Black body calibration spectrum Spectrometric and thermographic data |
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Infrared physics & technology |
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title |
A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility |
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title_full |
A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility |
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Savino, L. |
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Infrared physics & technology |
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Infrared physics & technology |
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eng |
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500 - Science |
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2020 |
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Savino, L. Martucci, A. Del Vecchio, A. De Cesare, M. |
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108 |
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Elektronische Aufsätze |
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Savino, L. |
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10.1016/j.infrared.2020.103353 |
dewey-full |
530 |
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verfasserin |
title_sort |
a novel physics methodology based on compact emission spectroscopy in the vnir (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the vnir – lwir (7–14 μm) ranges during atmospheric re-entry by pwt facility |
title_auth |
A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility |
abstract |
The following work reports a study that uses spontaneous emission spectroscopy for the evaluation of the average temperatures of the plasma shock layer and the test article surfaces subject to the hypersonic jet generated by the Plasma Wind Tunnel (PWT) facility at CIRA. Besides the qualitative information about the species of the hypersonic free stream emission generated by the SCIROCCO arcjet plasma tunnel, the most powerful PWT in the world, the main emission from the species in the shock layer can be obtained. |
abstractGer |
The following work reports a study that uses spontaneous emission spectroscopy for the evaluation of the average temperatures of the plasma shock layer and the test article surfaces subject to the hypersonic jet generated by the Plasma Wind Tunnel (PWT) facility at CIRA. Besides the qualitative information about the species of the hypersonic free stream emission generated by the SCIROCCO arcjet plasma tunnel, the most powerful PWT in the world, the main emission from the species in the shock layer can be obtained. |
abstract_unstemmed |
The following work reports a study that uses spontaneous emission spectroscopy for the evaluation of the average temperatures of the plasma shock layer and the test article surfaces subject to the hypersonic jet generated by the Plasma Wind Tunnel (PWT) facility at CIRA. Besides the qualitative information about the species of the hypersonic free stream emission generated by the SCIROCCO arcjet plasma tunnel, the most powerful PWT in the world, the main emission from the species in the shock layer can be obtained. |
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title_short |
A novel physics methodology based on compact emission spectroscopy in the VNIR (0.4–0.9 μm) ranges for plasma shock layer/material temperature determinations and surface emissivity evaluations in the VNIR – LWIR (7–14 μm) ranges during atmospheric re-entry by PWT facility |
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Martucci, A. Del Vecchio, A. De Cesare, M. |
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doi_str |
10.1016/j.infrared.2020.103353 |
up_date |
2024-07-06T22:17:19.383Z |
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