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Solar System Research

, Volume 52, Issue 7, pp 606–612 | Cite as

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
Article
  • 6 Downloads

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.

Keywords

CubeSat deorbiting 

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References

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Copyright information

© Pleiades Publishing, Inc. 2018

Authors and Affiliations

  • I. M. Nesterin
    • 1
  • K. M. Pichhadze
    • 2
  • V. K. Sysoev
    • 1
  • V. S. Finchenko
    • 1
  • S. O. Firsyuk
    • 2
  • A. D. Yudin
    • 1
  1. 1.Lavochkin AssociationKhimki, Moscow oblastRussia
  2. 2.Moscow Aviation InstituteNational Research UniversityMoscowRussia

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