Short electrodynamic tethers


Autoria(s): Sanmartín Losada, Juan Ramón; Ahedo Galilea, Eduardo; Conde López, Luis; Peláez Álvarez, Jesús; Ruiz, M.; Weinberger, M.; Hilgers, A.
Data(s)

2001

Resumo

ED bare theters are best systems to deorbit S/C at end of service. For near polar orbits, usual tethers kept vertical by the gravity gradient, yield too weak magnetic drag. Here we propose keeping tethers perpendicular to the orbital plane. they mus be rigid and short for structural reasons, requiring power supply like Ion thrusters. terher tube-booms that can be rolled up on a drum would lie on each side of the S/C. One boom, carying in idle Hollow Cathode, collects electrons; the opposite boom's HC ejects electrons.

Formato

application/pdf

Identificador

http://oa.upm.es/25611/

Idioma(s)

eng

Publicador

E.T.S.I. Aeronáuticos (UPM)

Relação

http://oa.upm.es/25611/1/C25.pdf

Direitos

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

info:eu-repo/semantics/openAccess

Fonte

A spacecraft charging Odyssey : proceedings of the spacecraft charging technology conference | 7th Spacecraft Charging Technology Conference | 23-27 apr | Noordwijk

Palavras-Chave #Aeronáutica #Física
Tipo

info:eu-repo/semantics/conferenceObject

Ponencia en Congreso o Jornada

NonPeerReviewed