Magnetic self-field effects on bare-tether current collection

Sanmartín Losada, Juan Ramón and Estes, Robert D. (2001). Magnetic self-field effects on bare-tether current collection. In: "7th Spacecraft Charging Technology Conference", 23-27 apr, Noordwijk. ISBN 92-9092-745-3.

Description

Title: Magnetic self-field effects on bare-tether current collection
Author/s:
  • Sanmartín Losada, Juan Ramón
  • Estes, Robert D.
Item Type: Presentation at Congress or Conference (Article)
Event Title: 7th Spacecraft Charging Technology Conference
Event Dates: 23-27 apr
Event Location: Noordwijk
Title of Book: A spacecraft charging Odyssey : proceedings of the spacecraft charging technology conference
Date: 2001
ISBN: 92-9092-745-3
Subjects:
Faculty: E.T.S.I. Aeronáuticos (UPM)
Department: Física Aplicada a la Ingeniería Aeronáutica [hasta 2014]
Creative Commons Licenses: Recognition - No derivative works - Non commercial

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Abstract

It has been recently suggested that the magnetic field created by the current in a bare tether could sensibly reduce its electron collection capability in the magnetised ionosphere, a region of closed magnetic surfaces disconnecting the cylinder from infinity. In this paper, the ohmic voltage drop along the tether is taken into account in considering self-field effects. Separate analyses are carried out for the thrust and power generation and drag modes of operation, which are affected in different ways. In the power generation and drag modes, bias decreases as current increases along the tether, starting at the anodic, positively-biased end (upper end in the usual, eastward-flying spacecraft); in the thrust mode of operation, bias increases as current increases along the tether, starting at the lower end. When the ohmic voltage drop is considered, self-field effects are shown to be weak, in all cases, for tape tethers, and for circular cross-section tethers just conductive in a thin outer layer. Self-field effects might become important, in the drag case only, for tethers with fully conductive cross sections that are unrealistically heavy.

More information

Item ID: 25610
DC Identifier: http://oa.upm.es/25610/
OAI Identifier: oai:oa.upm.es:25610
Deposited by: Biblioteca ETSI Aeronauticos
Deposited on: 25 Apr 2014 10:00
Last Modified: 22 Sep 2014 11:37
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