Deformation Characteristics of the Aerobraking Shell Material
- 作者: Rabinskii L.1, Medvedskii A.1, Nushtaev D.2, Lyskov D.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- OOO Tesis
- 期: 卷 2019, 编号 13 (2019)
- 页面: 1363-1368
- 栏目: 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
如何引用文章
详细
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.
作者简介
L. Rabinskii
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: rabinskiy@mail.ru
俄罗斯联邦, Moscow
A. Medvedskii
Moscow Aviation Institute (National Research University)
Email: rabinskiy@mail.ru
俄罗斯联邦, Moscow
D. Nushtaev
OOO Tesis
Email: rabinskiy@mail.ru
俄罗斯联邦, Moscow
D. Lyskov
Moscow Aviation Institute (National Research University)
Email: rabinskiy@mail.ru
俄罗斯联邦, Moscow
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