Numerical-experimental analysis of a carbon-phenolic composite via plasma jet ablation test
Pedro Guilherme Silva Pesci, Humberto Araújo Machado, Homero de Paula e Silva, Cristian Cley Paterniani Rita, Gilberto Petraconi Filho, Edson Cocchieri Botelho
ARTIGO
Inglês
Materials used in space vehicles components are subjected to thermally aggressive environments when exposed to atmospheric reentry. In order to protect the payload and the vehicle itself, ablative composites are employed as TPS (Thermal Protection System)
Fechado
Numerical-experimental analysis of a carbon-phenolic composite via plasma jet ablation test
Pedro Guilherme Silva Pesci, Humberto Araújo Machado, Homero de Paula e Silva, Cristian Cley Paterniani Rita, Gilberto Petraconi Filho, Edson Cocchieri Botelho
Numerical-experimental analysis of a carbon-phenolic composite via plasma jet ablation test
Pedro Guilherme Silva Pesci, Humberto Araújo Machado, Homero de Paula e Silva, Cristian Cley Paterniani Rita, Gilberto Petraconi Filho, Edson Cocchieri Botelho
Fontes
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Materials research express Vol. 5, no. 6 (June, 2018), n. art. 65601 |