Skip to main navigation Skip to search Skip to main content

Tether-nets for active space debris removal: Effect of the tether on deployment and capture dynamics

  • McGill University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

7 Scopus citations

Abstract

A promising method to mitigate the space debris problem is to actively capture and remove debris by means of tether-nets. The chaser-tether-net-debris system is modeled with rigid bodies connected by constraints; the tether can be spooled in and out by controlling a winch on the chaser. Through dynamics simulation, this paper analyzes the effect of the tether and its tensioning on net deployment and capture dynamics of space debris. This provides interesting insight into the preferred winching of the tether and into the feasibility of using the tether as a closing mechanism.

Original languageEnglish
Title of host publicationSpaceflight Mechanics 2017
EditorsJon A. Sims, Frederick A. Leve, Jay W. McMahon, Yanping Guo
PublisherUnivelt Inc.
Pages2003-2016
Number of pages14
ISBN (Print)9780877036371
StatePublished - 2017
Event27th AAS/AIAA Space Flight Mechanics Meeting, 2017 - San Antonio, United States
Duration: Feb 5 2017Feb 9 2017

Publication series

NameAdvances in the Astronautical Sciences
Volume160

Conference

Conference27th AAS/AIAA Space Flight Mechanics Meeting, 2017
Country/TerritoryUnited States
CitySan Antonio
Period02/5/1702/9/17

Fingerprint

Dive into the research topics of 'Tether-nets for active space debris removal: Effect of the tether on deployment and capture dynamics'. Together they form a unique fingerprint.

Cite this