Plasmas for space propulsion
By Eduardo Ahedo. 2011
188 citations recorded by the source corpus.
Subfields: Astronomy and Astrophysics, Electrical and Electronic Engineering, Nuclear and High Energy Physics
View Paper: https://www.semanticscholar.org/paper/f95493ffe9a9bc058e6d30766e9726b06180d1d8
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In Astronomy and Astrophysics
In Electrical and Electronic Engineering
- Jean-Pierre Boeuf
- Peter Bruggeman
- S. Starikovskaia
- K. Tachibana
- A. Gutsol
- Mark J. Kushner
- Anthony B. Murphy
- U. Kortshagen
In Nuclear and High Energy Physics
Citations in the corpus
- The 2012 Plasma Roadmap (2012, background): “Helicons can be efficient plasma sources for expansion through a magnetic nozzle, leading to an helicon thruster HelT ( [118], and IEPC-2005-290 in [119]).”
- Electric propulsion for satellites and spacecraft: established technologies and novel approaches (2016, methodology): “The regime of operation of an MPD thruster is therefore controlled by the plasma β parameter that corresponds to the ratio of the thermal to the magnetic pressure [10]”