Plasma-Surface Interactions in Hollow Cathode Discharges for Electric Propulsion

Plasma-Surface Interactions in Hollow Cathode Discharges for Electric Propulsion

<p>Electric thrusters generate high exhaust velocities and can achieve specific impulses in excess of 1000 s. The low thrust generation and high specific impulse make electric propulsion ideal for interplanetary missions, spacecraft station keeping, and orbit raising maneuvers. Consequently, t...

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Bibliographic Details
Main Author: Capece, Angela Maria
Format: Others
Language:en
Published: 2012
Online Access:https://thesis.library.caltech.edu/7108/4/Capece_Thesis_ChapterBib.pdf
Capece, Angela Maria (2012) Plasma-Surface Interactions in Hollow Cathode Discharges for Electric Propulsion. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/7TDQ-DR81. https://resolver.caltech.edu/CaltechTHESIS:05312012-113856351 <https://resolver.caltech.edu/CaltechTHESIS:05312012-113856351>

Internet

https://thesis.library.caltech.edu/7108/4/Capece_Thesis_ChapterBib.pdf
Capece, Angela Maria (2012) Plasma-Surface Interactions in Hollow Cathode Discharges for Electric Propulsion. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/7TDQ-DR81. https://resolver.caltech.edu/CaltechTHESIS:05312012-113856351 <https://resolver.caltech.edu/CaltechTHESIS:05312012-113856351>

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