Using Small Satellites to Remove Non-Cooperative Space Debris

  • Virupakshan Vilvanathan
  • , Athip Thirupathi Raj
  • , Sivaperuman Muniyasamy
  • , Vivek Verma
  • , Jekan Thangavelautham

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Advancements in Small Satellite technologies have allowed for an increase in the number of satellites in orbit around the earth. Unfortunately, this also means that this has led to an increase in space debris in orbit around the earth. Space debris, if left unattended, can pose a severe threat to near-earth activities and therefore needs to be mitigated urgently. To address this problem, we suggest a small satellite system capable of active space debris removal through “grouping and clumping” together of space debris using rendezvous and docking operations. We propose using an electromagnetic system in tandem with an inflatable system. These systems will enable docking with a space debris object and pulling it out of orbit, thereby clearing the orbit of space debris. We suggest using electromagnets because a magnetic field will ensure a stable storage position and allow the small satellite to attach or detach at will. This mechanism may be achieved by including ratiometric and proximity sensors. The electromagnetic system will be capable of attaching itself to the debris and staying locked to the object’s wall until it is necessary to release the object. The inflatable system will slow down the object to allow a soft capture of the space debris and also deploy a drag area once in a position to move the debris out of orbit. The inflatable system will consist of gasses such as N2 (Nitrogen) that can be reused for as many operations as the small satellite needs to accomplish. The system can then reuse the gas by absorbing it back into tanks once the debris has been captured/secured. The small satellite will then use the same inflatable to enter the earth’s atmosphere to avoid contributing to existing space debris. This paper constructs system and subsystem requirements for such a small satellite system and explores their key enabling technologies. We also discuss potential risk factors and mitigation measures necessary to implement this technology in space applications.

Original languageEnglish (US)
Title of host publicationAccelerating Space Commerce, Exploration, and New Discovery conference, ASCEND 2022
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106620
DOIs
StatePublished - 2022
Externally publishedYes
EventAccelerating Space Commerce, Exploration, and New Discovery conference, ASCEND 2022 - Las Vegas, United States
Duration: Oct 24 2022Oct 26 2022

Publication series

NameAccelerating Space Commerce, Exploration, and New Discovery conference, ASCEND 2022

Conference

ConferenceAccelerating Space Commerce, Exploration, and New Discovery conference, ASCEND 2022
Country/TerritoryUnited States
CityLas Vegas
Period10/24/2210/26/22

Keywords

  • Commercial off the Shelf
  • Earth
  • Earth Atmosphere
  • Electrodynamic Tether
  • Inflatable Structures
  • Proximity Sensors
  • Satellite Technology
  • Small Satellites
  • Space Debris

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

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