Electrodynamic tethers for spacecraft propulsion

Johnson, L. and Estes, Robert D. and Lorenzini, Enrico C. and Martínez-Sánchez, Manuel and Sanmartín Losada, Juan Ramón and Vas, I.E. (1998). Electrodynamic tethers for spacecraft propulsion. In: "36th Aerospace Sciences Meeting & Exhibit", 12 - 15 Jan 1998, Reno, Nevada.


Title: Electrodynamic tethers for spacecraft propulsion
  • Johnson, L.
  • Estes, Robert D.
  • Lorenzini, Enrico C.
  • Martínez-Sánchez, Manuel
  • Sanmartín Losada, Juan Ramón
  • Vas, I.E.
Item Type: Presentation at Congress or Conference (Article)
Event Title: 36th Aerospace Sciences Meeting & Exhibit
Event Dates: 12 - 15 Jan 1998
Event Location: Reno, Nevada
Title of Book: 36th Aerospace Sciences Meeting & Exhibit
Date: 1998
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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Relatively short electrodynamic tethers can use solar power to "push" against a planetary magnetic field to achieve propul sion without expenditure of propellant. The groundwork has been laid for this type of propulsion. Recent important milestones include retrieval of a tether in space (TSS-1, 1992), successful deployment of a 20-km-long tether in space (SEDS-1, 1993), and operation of an electrodynamic tether with tether current driven in both directions (PMG, 1993). The planned Propulsive Small Expendable Deployer System (ProSEDS) experiment will use the flight-proven Small Expendable Deployer System (SEDS) to deploy a 5-km bare copper tether from a Delta II upper stage to achieve -0,4 N drag thrust, thus deorbiting the stage, The experiment will use a predominantly "bare" tether for current collection in lieu of the endmass collector and insulated tether approach used on previous missions, Theory and ground-based plasma chamber testing indicate that the bare tether is a highly efficient current collector. The flight experiment is a precursor to utilization of the technology on the International Space tation (JSS) for reboost and the electrodynamic tether pper stage demonstration misión which will be capable of orbit raising, lowering, and inclination changes—all using electrodynamic thrust. In addition, the use of this type of propulsion may be attractive for future missions to Jupiter.

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Item ID: 31234
DC Identifier: http://oa.upm.es/31234/
OAI Identifier: oai:oa.upm.es:31234
Deposited by: Biblioteca ETSI Aeronauticos
Deposited on: 03 Oct 2014 12:28
Last Modified: 03 Oct 2014 12:28
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