The numerical simulation and the measurement of electromagnetic shielding at microwave frequencies of thermal protection system for hypersonic vehicles is presented using nested reverberation chamber. An example of a possible thermal protection system for a re-entry vehicle is presented. This system based on carbon material is electromagnetically characterized. The characterization takes into account not only the materials but also the final assembly configuration of the thermal protection system. The frequency range is 2-8 GHz. The results of measurements and simulations show that the microwave shielding effectiveness of carbon materials is above 60 dB for a single tile and that the tile inter-distance is able to downgrade the shielding effectiveness on the average to about 40 dB. (C) 2013 IAA. Published by Elsevier Ltd. All rights reserved.

Electromagnetic shielding of thermal protection system for hypersonic vehicles / Albano, Marta; Micheli, Davide; G., Gradoni; R. B., Morles; Marchetti, Mario; F., Moglie; V., Mariani Primiani. - In: ACTA ASTRONAUTICA. - ISSN 0094-5765. - STAMPA. - 87:(2013), pp. 30-39. [10.1016/j.actaastro.2013.02.003]

Electromagnetic shielding of thermal protection system for hypersonic vehicles

ALBANO, MARTA;MICHELI, DAVIDE;MARCHETTI, Mario;
2013

Abstract

The numerical simulation and the measurement of electromagnetic shielding at microwave frequencies of thermal protection system for hypersonic vehicles is presented using nested reverberation chamber. An example of a possible thermal protection system for a re-entry vehicle is presented. This system based on carbon material is electromagnetically characterized. The characterization takes into account not only the materials but also the final assembly configuration of the thermal protection system. The frequency range is 2-8 GHz. The results of measurements and simulations show that the microwave shielding effectiveness of carbon materials is above 60 dB for a single tile and that the tile inter-distance is able to downgrade the shielding effectiveness on the average to about 40 dB. (C) 2013 IAA. Published by Elsevier Ltd. All rights reserved.
2013
carbon foam; carbon silicon carbide; carbon/carbon; electromagnetic shielding effectiveness; numerical simulation; reverberation chamber; space re-entry vehicle; thermal protection system
01 Pubblicazione su rivista::01a Articolo in rivista
Electromagnetic shielding of thermal protection system for hypersonic vehicles / Albano, Marta; Micheli, Davide; G., Gradoni; R. B., Morles; Marchetti, Mario; F., Moglie; V., Mariani Primiani. - In: ACTA ASTRONAUTICA. - ISSN 0094-5765. - STAMPA. - 87:(2013), pp. 30-39. [10.1016/j.actaastro.2013.02.003]
File allegati a questo prodotto
Non ci sono file associati a questo prodotto.

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/508708
 Attenzione

Attenzione! I dati visualizzati non sono stati sottoposti a validazione da parte dell'ateneo

Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 76
  • ???jsp.display-item.citation.isi??? 68
social impact