Email this article Deformation Characteristics of the Aerobraking Shell Material
- Authors: Rabinskii L.N.1, Medvedskii A.L.1, Nushtaev D.V.2, Lyskov D.V.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- OOO Tesis
- Issue: Vol 2019, No 13 (2019)
- Pages: 1363-1368
- Section: 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
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Abstract
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.
About the authors
L. N. Rabinskii
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: rabinskiy@mail.ru
Russian Federation, Moscow
A. L. Medvedskii
Moscow Aviation Institute (National Research University)
Email: rabinskiy@mail.ru
Russian Federation, Moscow
D. V. Nushtaev
OOO Tesis
Email: rabinskiy@mail.ru
Russian Federation, Moscow
D. V. Lyskov
Moscow Aviation Institute (National Research University)
Email: rabinskiy@mail.ru
Russian Federation, Moscow
