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


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Abstract

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.

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About the authors

I. M. Nesterin

Lavochkin Association

Author for correspondence.
Email: nesterin@laspace.ru
Russian Federation, Khimki, Moscow oblast, 141402

K. M. Pichhadze

Moscow Aviation Institute

Email: nesterin@laspace.ru
Russian Federation, Moscow, 125993

V. K. Sysoev

Lavochkin Association

Email: nesterin@laspace.ru
Russian Federation, Khimki, Moscow oblast, 141402

V. S. Finchenko

Lavochkin Association

Email: nesterin@laspace.ru
Russian Federation, Khimki, Moscow oblast, 141402

S. O. Firsyuk

Moscow Aviation Institute

Email: nesterin@laspace.ru
Russian Federation, Moscow, 125993

A. D. Yudin

Lavochkin Association

Email: nesterin@laspace.ru
Russian Federation, Khimki, Moscow oblast, 141402

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