Design Experience of a Demonstrator Descent Vehicle Introducing Aeroelastic Deployable Structural Elements to Space Engineering
- 作者: Alifanov O.M.1, Medvedskiy A.L.1, Terentyev V.V.1, Lyskov D.V.1
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隶属关系:
- Moscow Aviation Institute
- 期: 卷 52, 编号 7 (2018)
- 页面: 590-596
- 栏目: Article
- URL: https://journals.rcsi.science/0038-0946/article/view/171137
- DOI: https://doi.org/10.1134/S0038094618070031
- ID: 171137
如何引用文章
详细
The development project of a prototype demonstrator for a descent vehicle and the possibilities of descent from orbit using aero-elastic braking devices deployable in space and in the atmosphere is considered. The project was carried out jointly by the Lavochkin Scientific Production Association and the Moscow Aviation Institute teams in 2013–2015. The results are evaluated for both the project itself and the cooperation of the two organizations.
作者简介
O. Alifanov
Moscow Aviation Institute
编辑信件的主要联系方式.
Email: nio6@mai.ru
俄罗斯联邦, Moscow, 125993
A. Medvedskiy
Moscow Aviation Institute
Email: nio6@mai.ru
俄罗斯联邦, Moscow, 125993
V. Terentyev
Moscow Aviation Institute
Email: nio6@mai.ru
俄罗斯联邦, Moscow, 125993
D. Lyskov
Moscow Aviation Institute
Email: nio6@mai.ru
俄罗斯联邦, Moscow, 125993
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