Design Experience of a Demonstrator Descent Vehicle Introducing Aeroelastic Deployable Structural Elements to Space Engineering
- Autores: Alifanov O.M.1, Medvedskiy A.L.1, Terentyev V.V.1, Lyskov D.V.1
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Afiliações:
- Moscow Aviation Institute
- Edição: Volume 52, Nº 7 (2018)
- Páginas: 590-596
- Seção: Article
- URL: https://journal-vniispk.ru/0038-0946/article/view/171137
- DOI: https://doi.org/10.1134/S0038094618070031
- ID: 171137
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Resumo
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.
Sobre autores
O. Alifanov
Moscow Aviation Institute
Autor responsável pela correspondência
Email: nio6@mai.ru
Rússia, Moscow, 125993
A. Medvedskiy
Moscow Aviation Institute
Email: nio6@mai.ru
Rússia, Moscow, 125993
V. Terentyev
Moscow Aviation Institute
Email: nio6@mai.ru
Rússia, Moscow, 125993
D. Lyskov
Moscow Aviation Institute
Email: nio6@mai.ru
Rússia, Moscow, 125993
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