Proposal for Creating a Device for Deorbiting Low-Earth-Orbit CubeSats

I. M. Nesterin; K. M. Pichhadze; V. K. Sysoev; V. S. Finchenko; S. O. Firsyuk; A. D. Yudin

doi:10.1134/S003809461807016X

Proposal for Creating a Device for Deorbiting Low-Earth-Orbit CubeSats

Autores: Nesterin I.M.¹, Pichhadze K.M.², Sysoev V.K.¹, Finchenko V.S.¹, Firsyuk S.O.², Yudin A.D.¹
Afiliações:
1. Lavochkin Association
2. Moscow Aviation Institute
Edição: Volume 52, Nº 7 (2018)
Páginas: 606-612
Seção: Article
URL: https://journals.rcsi.science/0038-0946/article/view/171146
DOI: https://doi.org/10.1134/S003809461807016X
ID: 171146

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The article discusses proposals for creating a standard unit based on CubeSat technology, an independent autonomous aerobraking device based on inflatable balloons or a solar sail cone section. The proposed devices have a simple start-up system and are an additional component in the CubeSat assembly for deorbiting from low-Earth orbits.