Zobrazeno 1 - 10
of 20
pro vyhledávání: '"De Stefano Fumo, Mario"'
Autor:
Novembre, Edoardo, Airoldi, Alessandro, Riva, Marco, Caporale, Antonio Maria, Cavalli, Lorenzo, De Stefano Fumo, Mario
Publikováno v:
In Journal of the European Ceramic Society October 2024 44(13):7490-7503
Autor:
Riva, Marco, Airoldi, Alessandro, Caporale, Antonio Maria, Cavalli, Lorenzo, De Stefano Fumo, Mario
Publikováno v:
In Composites Part A December 2023 175
Publikováno v:
In Corrosion Science 2011 53(3):922-929
Autor:
Savino, Raffaele, De Stefano Fumo, Mario, Paterna, Diego, Di Maso, Andrea, Monteverde, Frederic
Publikováno v:
In Aerospace Science and Technology 2010 14(3):178-187
Autor:
Brunello, Alice, Valmorbida, Andrea, Lorenzini, Enrico C., Cantoni, Stefania, De Stefano Fumo, Mario, Fedele, Alberto, Gardi, Roberto, Votta, Raffaele
Publikováno v:
CEAS Space Journal; Apr2021, Vol. 13 Issue 2, p217-230, 14p
Autor:
DE STEFANO FUMO, Mario, SCIGLIANO, Roberto, BELARDO, Marika, RUFOLO, Giuseppe, ESPOSITO, Angelo, LINARI, Mauro
Hot structures made of Ceramic Matrix Composites (CMC) for space re-entry vehicles play a key role regarding the feasibility of advanced and reusable space transportation systems. In particular, looking to IXV experience and SPACE RIDER requirements,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1d0d4a9c554746f9fcf390cd934972e5
Autor:
BELARDO, Marika, DE STEFANO FUMO, Mario, SPENA, Paola, SCIGLIANO, Roberto, MARINO, GIULIANO, CANTONI, Stefania, CAVALLI, Lorenzo, VALLE, Max
Re-entry systems are subject to the harsh environment during hypersonic atmospheric re-entry phase. In order to withstand the high aerothermal loads, thermal protections systems are necessary to protect the vehicle and hot structures are mandatory fo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::10c5de94bae0900b91886d68a4fa46c0
Publikováno v:
3 (2010): 10–19.
info:cnr-pdr/source/autori:Di Maso A.; Savino R.; De Stefano Fumo M.; Silvestroni L.; Sciti D./titolo:Arc-Jet Testing on HfB2-TaSi2 Models: Effect of the Geometry on the Aerothermal Behaviour/doi:/rivista:/anno:2010/pagina_da:10/pagina_a:19/intervallo_pagine:10–19/volume:3
info:cnr-pdr/source/autori:Di Maso A.; Savino R.; De Stefano Fumo M.; Silvestroni L.; Sciti D./titolo:Arc-Jet Testing on HfB2-TaSi2 Models: Effect of the Geometry on the Aerothermal Behaviour/doi:/rivista:/anno:2010/pagina_da:10/pagina_a:19/intervallo_pagine:10–19/volume:3
Arc-jet experiments in high enthalpy hypersonic (Mach 3) non equilibrium flow were carried out on a HfB2 composite with addition of 15 vol% TaSi2, at temperatures exceeding 2000 K. The aerothermal behaviour was tested considering models having two di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::edd528084d6e4ca22eaab2b063e04035
http://www.cnr.it/prodotto/i/68221
http://www.cnr.it/prodotto/i/68221
Publikováno v:
MRS Online Proceedings Library; 2004, Vol. 851 Issue 1, p127-132, 6p