Skip to main content

The Shuttle Electrodynamic Tether Mission

  • Chapter
Environmental and Space Electromagnetics
  • 266 Accesses

Abstract

The Tethered Satellite System (TSS) is a Shuttle-based facility being developed by NASA and the Italian Space Agency under a cooperative agreement. The joint development work began in 1984, and the first TSS mission is currently manifested in the fall of 1991. Its main objective is to verify the capability of the facility to deploy, control, and retrieve a tethered satellite. Additionally, the mission will demonstrate the electrodynamic science capability of the system and perform various scientific experiments. The instrumentation, the scientific objectives, and the planned investigations are summarized; references are given to more detailed accounts.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 84.99
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 109.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Grossi, M.D., and Columbo, G. (1978). Interactions of a tethered satellite system with the ionosphere. In: Wu, S.T. (ed), Proceedings of the University of Alabama/NASA Workshop on the Uses of a Tethered Satellite System, University of Alabama, Huntsville.

    Google Scholar 

  2. Williamson, P.R., Banks, P.M., and Oyama, K. (1978). The electrodynamic tether. In: Wu, S.T. (ed), Proceedings of the University of Alabama/NASA Workshop on the Uses of a Tethered Satellite System, University of Alabama, Huntsville.

    Google Scholar 

  3. Banks, P.M., Williamson, P.R., and Oyama, K.-I. (1981). Electrical behavior of a Shuttle electrodynamic tether system (SETS), Planet. Space Sci. 29: 139–147.

    Article  Google Scholar 

  4. Stenzel, R.L., and Urrutia, J.M., (1990). Currents between tethered electrodes in a magnetized laboratory plasma, J. Geophys. Res. 95: 6209–6226.

    Article  Google Scholar 

  5. Barnett, A., and Olbert, S. (1986). Radiation of plasma waves by a conducting body moving through a magnetized plasma, J. Geophys. Res. 91: 10, 117–135.

    Google Scholar 

  6. Estes, R.D. (1988). Alfven waves from an electrodynamic tethered satellite system, J. Geophys. Res. 93: 945–956.

    Article  Google Scholar 

  7. Newell, P.T. (1985). Review of the critical ionization velocity effect in space, Rev. Geophys. 23: 93–104.

    Article  Google Scholar 

  8. Formisano,V., Galeev, A.A., and Sagdeev, R.Z. (1982). The role of the critical ionization velocity phenomena in the production of inner coma cometary plasma, Planet. Space Sci. 30: 491–497.

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 1991 Springer-Verlag Tokyo

About this chapter

Cite this chapter

Storey, L.R.O. (1991). The Shuttle Electrodynamic Tether Mission. In: Kikuchi, H. (eds) Environmental and Space Electromagnetics. Springer, Tokyo. https://doi.org/10.1007/978-4-431-68162-5_2

Download citation

  • DOI: https://doi.org/10.1007/978-4-431-68162-5_2

  • Publisher Name: Springer, Tokyo

  • Print ISBN: 978-4-431-68164-9

  • Online ISBN: 978-4-431-68162-5

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics