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Propellantless deorbiting of space debris by bare electrodynamic tethers

  • Juan R. Sanmartin*
  • , Shaker B. Khan
  • , Claudio Bombardelli
  • , Enrico C. Lorenzini
  • , Giacomo Colombatti
  • , Denis Zanutto
  • , Jean Francois Roussel
  • , Pierre Sarrailh
  • , John D. Williams
  • , Garrett E. Metz
  • , James K. Thomas
  • , Jose A. Carrasco
  • , Francisco Garcia De Quiros
  • , Olaf Kroemer
  • , Roland Rosta
  • , Tim Van Zoest
  • , Joseba Lasa
  • , Jesus Marcos
  • *Autor correspondiente de este trabajo

Producción científica: Capítulo del libro/informe/acta de congresoContribución a la conferenciarevisión exhaustiva

3 Citas (Scopus)

Resumen

A 3-year Project started on November 1 2010, financed by the European Commision within the FP-7 Space Program, and aimed at developing an efficient de-orbit system that could be carried on board by future spacecraft launched into LEO, will be presented. The operational system will deploy a thin uninsulated tape-tether to collect electrons as a giant Langmuir probe, using no propellant/no power supply, and generating power on board. This project will involve free-fall tests, and laboratory hypervelocity-impact and tether-current tests, and design/Manufacturing of subsystems: interface elements, electric control and driving module, electron-ejecting plasma contactor, tether-deployment mechanism/end-mass, and tape samples. Preliminary results to be presented involve: i) devising criteria for sizing the three disparate tape dimensions, affecting mass, resistance, current-collection, magnetic self-field, and survivability against debris itself; ii) assessing the dynamical relevance of tether parameters in implementing control laws to limit oscillations in /off the orbital plane, where passive stability may be marginal; iii) deriving a law for bare-tape current from numerical simulations and chamber tests, taking into account ambient magnetic field, ion ram motion, and adiabatic electron trapping; iv) determining requirements on a year-dormant hollow cathode under long times/broad emission-range operation, and trading-off against use of electron thermal emission; v) determining requirements on magnetic components and power semiconductors for a control module that faces high voltage/power operation under mass/volume limitations; vi) assessing strategies to passively deploy a wide conductive tape that needs no retrieval, while avoiding jamming and ending at minimum libration; vii) evaluating the tape structure as regards conductive and dielectric materials, both lengthwise and in its cross-section, in particular to prevent arcing in triple-point junctions.

Idioma originalInglés
Título de la publicación alojada62nd International Astronautical Congress 2011, IAC 2011
Páginas2239-2248
Número de páginas10
EstadoPublicada - 2011
Evento62nd International Astronautical Congress 2011, IAC 2011 - Cape Town, Sudáfrica
Duración: 3 oct 20117 oct 2011

Serie de la publicación

Nombre62nd International Astronautical Congress 2011, IAC 2011
Volumen3

Conferencia

Conferencia62nd International Astronautical Congress 2011, IAC 2011
País/TerritorioSudáfrica
CiudadCape Town
Período3/10/117/10/11

ODS de las Naciones Unidas

Este resultado contribuye a los siguientes Objetivos de Desarrollo Sostenible

  1. ODS 9: Industria, innovación e infraestructura
    ODS 9: Industria, innovación e infraestructura

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