A joint research work financed by CIRA and performed with the support of the CNR-ISTEC have been performed with the aim to evaluate and to assess the use of non-conventional metal diboride compounds in the manufacturing of slender-shaped hot structures for re-entry vehicles. The results of the metal diborides trade-off and the characterisation of the selected material are reported in this paper. A description of the material process employed is also provided. Different diboride compositions, both hafnium- and zirconium- based, have been considered and characterized in their mechanical, thermal and oxidation resistance behaviour: as a result of this trade-off, the most promising composition was chosen and further characterised. The obtained results highlight an excellent potential for the selected material. A scaled hot structure demonstrator, to be on-ground tested at CIRA Scirocco Plasma Wind Tunnel, have also been manufactured.

Characterization and process of new metal diboride compound for TPS applications

A Bellosi;F Monteverde
2005

Abstract

A joint research work financed by CIRA and performed with the support of the CNR-ISTEC have been performed with the aim to evaluate and to assess the use of non-conventional metal diboride compounds in the manufacturing of slender-shaped hot structures for re-entry vehicles. The results of the metal diborides trade-off and the characterisation of the selected material are reported in this paper. A description of the material process employed is also provided. Different diboride compositions, both hafnium- and zirconium- based, have been considered and characterized in their mechanical, thermal and oxidation resistance behaviour: as a result of this trade-off, the most promising composition was chosen and further characterised. The obtained results highlight an excellent potential for the selected material. A scaled hot structure demonstrator, to be on-ground tested at CIRA Scirocco Plasma Wind Tunnel, have also been manufactured.
2005
Istituto di Scienza, Tecnologia e Sostenibilità per lo Sviluppo dei Materiali Ceramici - ISSMC (ex ISTEC)
International Space Planes and Hypersonic Systems and Technologies Conferences AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference
13th International Space Planes and Hypersonics Systems and Technologies
2005-3267
1
8
8
978-1-62410-068-0
No
17-20/5/2005
Capua
UHTC
plasma wind tunnel
2
none
L. Scatteia; R. Borrelli; G. Marino; A. Bellosi; F. Monteverde
273
info:eu-repo/semantics/conferenceObject
04 Contributo in convegno::04.01 Contributo in Atti di convegno
File in 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/20.500.14243/101671
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus ND
  • ???jsp.display-item.citation.isi??? ND
social impact