Propellantless de orbiting of space debris by bare electrodynamic tethers


Autoria(s): Sanmartín Losada, Juan Ramón; Kahn, Saker B.; Bombardelli, Claudio; Lorenzini, Enrico C.; Colombatti, Giacomo; Zanutto, Denis; Roussel, Jean-François; Sarrailh, Pierre; Williams, John D.; Metz, Garret E.; Thomas, James K.; Carrasco, José A.; García de Quirós, Francisco; Kroemer, Olaf; Rosta, Roland; Zoest, Tim van; Lasa, Joseba; Marcos, Jesús
Data(s)

2011

Resumo

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.

Formato

application/pdf

Identificador

http://oa.upm.es/26064/

Idioma(s)

eng

Publicador

E.T.S.I. Aeronáuticos (UPM)

Relação

http://oa.upm.es/26064/1/C35a.pdf

Direitos

http://creativecommons.org/licenses/by-nc-nd/3.0/es/

info:eu-repo/semantics/openAccess

Fonte

62nd International Astronautical Congress | 62nd International Astronautical Congress | 3-7 oct 2010 | Cape Twon, Sudafrica

Palavras-Chave #Aeronáutica #Física
Tipo

info:eu-repo/semantics/conferenceObject

Ponencia en Congreso o Jornada

PeerReviewed