Enviar artigo por via de e-mail Deformation Characteristics of the Aerobraking Shell Material
- Autores: Rabinskii L.1, Medvedskii A.1, Nushtaev D.2, Lyskov D.1
-
Afiliações:
- Moscow Aviation Institute (National Research University)
- OOO Tesis
- Edição: Volume 2019, Nº 13 (2019)
- Páginas: 1363-1368
- Seção: New Materials. Technology of Composite Materials
- URL: https://journals.rcsi.science/0036-0295/article/view/173811
- DOI: https://doi.org/10.1134/S0036029519130299
- ID: 173811
Citar
Acesso aberto
Acesso está concedido
Somente assinantes
Resumo
The deformation characteristics of silica fabric with a thermal barrier coating, which is used for the production of the ballute-type aerobrake of a descent module, are estimated. A rubberized fabric strip is subjected to uniaxial tensile tests to failure. Various finite-element simulation approaches to the deformation of the fabric are considered.
Sobre autores
L. Rabinskii
Moscow Aviation Institute (National Research University)
Autor responsável pela correspondência
Email: rabinskiy@mail.ru
Rússia, Moscow
A. Medvedskii
Moscow Aviation Institute (National Research University)
Email: rabinskiy@mail.ru
Rússia, Moscow
D. Nushtaev
OOO Tesis
Email: rabinskiy@mail.ru
Rússia, Moscow
D. Lyskov
Moscow Aviation Institute (National Research University)
Email: rabinskiy@mail.ru
Rússia, Moscow
