2020
DOI: 10.1016/j.paerosci.2019.06.001
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Applied radiation physics techniques for diagnostic evaluation of the plasma wind and thermal protection system critical parameters in aerospace re-entry

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Cited by 30 publications
(8 citation statements)
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“…Furthermore, the DC technique has to be used in applications where the emissivity of the materials is not well known, such as in the case of the test performed in the PWT facilities to verify the TPS withstanding the hypersonic plasma interactions [12][13][14][15]. Before testing the methodology in the PWT aerospace field, the Center for Isotopic Research on the Cultural and Environmental heritage (CIRCE) accelerator [16][17][18][19], upgraded both to perform accelerator mass spectrometry (AMS) up to actinides [20][21][22][23][24] and for experimental nuclear astrophysics [25][26][27][28][29][30][31][32] as other AMS systems [33], can be used for the preliminary test at temperature values reaching 1500 • C, with materials that, at the beginning of the process, are characterized by a low emissivity, and increase their emissivity value with a carbon ions implantation.…”
Section: Results and Conclusionmentioning
confidence: 99%
“…Furthermore, the DC technique has to be used in applications where the emissivity of the materials is not well known, such as in the case of the test performed in the PWT facilities to verify the TPS withstanding the hypersonic plasma interactions [12][13][14][15]. Before testing the methodology in the PWT aerospace field, the Center for Isotopic Research on the Cultural and Environmental heritage (CIRCE) accelerator [16][17][18][19], upgraded both to perform accelerator mass spectrometry (AMS) up to actinides [20][21][22][23][24] and for experimental nuclear astrophysics [25][26][27][28][29][30][31][32] as other AMS systems [33], can be used for the preliminary test at temperature values reaching 1500 • C, with materials that, at the beginning of the process, are characterized by a low emissivity, and increase their emissivity value with a carbon ions implantation.…”
Section: Results and Conclusionmentioning
confidence: 99%
“…2016;Eckbreth 1996) and review articles (Miles and Lempert 1997;Miles 2015;Ehn et al. 2017;De Cesare et al 2020,). Of particular relevance for the application of these diagnostics to hypersonic flows is a recent NATO review article that addresses absorption spectroscopy, planar laserinduced fluorescence (PLIF), molecular tagging velocimetry (MTV), focused laser differential interferometry (FLDI), light scattering (Rayleigh and Raman), coherent anti-Stokes Raman scattering (CARS), particle imaging velocimetry (PIV) and optical emission spectroscopy (OES) (Danehy et al 2019).…”
Section: Introductionmentioning
confidence: 99%
“…requires sensitive and accurate tests to be performed at conditions as close as possible to those during a space vehicle's re-entry: this can be done in facilities like plasma wind tunnels (PWTs) [3,4]. Present methods employed to measure samples recession rates (extensively discussed in a recent review [3]), which is the most widely employed parameter to compare TPS performances, rely either on the measurement of the sample length before and after the test, on the insertion of intrusive break-wire sensors or on non-intrusive optical and spectroscopic techniques. The first is an off-line method which give no hints on what happens during the test, the second is intrusive and can reduce results accuracy and the latter have low sensitivity [3].…”
Section: Introduction: Recession Measurements For Aerospacementioning
confidence: 99%