Results of the qualification test campaign of a Pulsed Plasma Thruster for Cubesat Propulsion (PPTCUP)

Pulsed Plasma Thruster for Cubesat Propulsion (PPTCUP) is an ablative pulsed plasma thruster designed with the aim of providing translational and orbital control to Cubesat platforms. The qualification model presented in this paper has been developed by Mars Space Ltd, Clyde Space Ltd and the Univer...

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Bibliographic Details
Main Authors: Ciaralli, S. (Author), Coletti, M. (Author), Gabriel, S.B (Author)
Format: Article
Language:English
Published: 2016-04.
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