Increased Thrust-to-Power Ratio of a Stepped-Diameter Helicon Plasma Thruster with Krypton Propellant
Journal of Propulsion and Power ; 36 , 6 ; 961-965
01.11.2020
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
A Solid Propellant High Power Helicon Thruster
AIAA | 2016
|A SOLID PROPELLANT HIGH POWER HELICON THRUSTER (AIAA 2016-4736)
British Library Conference Proceedings | 2016
|AIAA | 2005
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