Deformation Characteristics of the Aerobraking Shell Material


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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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