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Flowing Plasma Interaction with an Electric Sail Tether ElementHarnessing the power of the solar wind, an Electric Sail, or E-sail, is a relatively new concept that promises to deliver high speed propellant-less propulsion. The electric sail is an invention made in 2006 at the Kumpula Space Centre in Finland by Pekka Janhunen [Janhunen and Sandroos, 2007]. At its core, an electric sail utilizes multiple positively biased tethers which exchange momentum with solar wind protons via the repelling electric field established around each tether, in other words, by reflecting the solar wind protons. Recognizing the solar wind is a plasma, the effective repelling area of each tether is increased significantly by the formation a plasma sheath around each tether. Fig. 1 shows schematically a spacecraft employing an electric sail. The positive voltage bias (greater than10kV) applied to each tether naturally results in electron collection. Therefore, the electric sail concept necessarily includes an electron source (electron gun) to return collected electrons to space and maintain the positive bias of the tether system.
Document ID
20170005318
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Schneider, Todd
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Vaughn, Jason
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Wright, Kenneth
(Universities Space Research Association Boulder, CO, United States)
Anderson, Allen
(Utah State Univ. Logan, UT, United States)
Stone, Nobie
(ManTech NeXolve Corp. United States)
Date Acquired
June 7, 2017
Publication Date
May 15, 2017
Subject Category
Plasma Physics
Spacecraft Propulsion And Power
Report/Patent Number
M17-6019
Meeting Information
Meeting: Applied Space Environments Conference (ASEC) 2017
Location: Huntsville, AL
Country: United States
Start Date: May 15, 2017
End Date: May 19, 2017
Sponsors: Universities Space Research Association
Distribution Limits
Public
Copyright
Public Use Permitted.
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