The work investigates the effect of new components on the Helicon plasma thruster under development at CISAS (Center of Studies and Activities for Space, University of Padova) propulsion laboratory;then define a method to calculate a correction coefficient for Faraday cup that may be used to compute thrust.Eventually, a suggestion for improve for actual Faraday cup is given
Analysis and design of plasma thruster plume
Grezzani, Andrea
2014/2015
Abstract
The work investigates the effect of new components on the Helicon plasma thruster under development at CISAS (Center of Studies and Activities for Space, University of Padova) propulsion laboratory;then define a method to calculate a correction coefficient for Faraday cup that may be used to compute thrust.Eventually, a suggestion for improve for actual Faraday cup is givenFile in questo prodotto:
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TESI_ANDREA_GREZZANI.pdf
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Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/19187