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Flowing Plasma Interaction with an Electric Sail Tether ElementElectric sails are a relatively new concept for providing high speed propellant-less propulsion. Employing multiple tethers biased to high positive voltage levels (kV), electric sails are designed to gain momentum from the solar wind by repelling solar wind protons. To maximize the area of the sail that interacts with the solar wind, electric sails rely on the formation of a large plasma sheath around each small diameter tether. Motivated by interest in advancing the development of electric sails, a set of laboratory tests has been conducted to study the interaction of a drifting plasma with a sheath formed around a small diameter tether element biased at positive voltages. The laboratory test setup was created with Debye length scaling in mind to offer a path to extrapolate (via modeling) to full scale electric sail missions. Using an instrument known as a Differential Ion Flux Probe (DIFP) the interaction between a positively biased tether element and a drifting plasma has been measured for several scenarios. Clear evidence of the tether element sheath deflecting ions has been obtained. Maps of the flow angle downstream from the tether element have been made and they show the influence of the plasma sheath. Finally, electron current collection measurements have been made for a wide range of plasma conditions and tether element bias voltages. The electron collection data will have an impact on electric sail power requirements, as high voltage power supplies and electron guns will have to be sized to accommodate the electron currents collected by each tether.
Document ID
20170008055
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 Huntsville, AL, United States)
Andersen, Allen
(Utah State Univ. Logan, UT, United States)
Stone, Nobie
(NeXolve, Inc. Huntsville, AL, United States)
Date Acquired
August 30, 2017
Publication Date
May 15, 2017
Subject Category
Solar 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: NASA Headquarters
Distribution Limits
Public
Copyright
Public Use Permitted.
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