Hall Effect Thruster Direct Drive PPUs, Experimental Investigation of the Cathode Potential Grounding Problem
| Autor: | Luca Ghislanzoni, Luca Benetti, Lorenzo Fontani, Tommaso Misuri, Giovanni Cesaretti |
|---|---|
| Rok vydání: | 2017 |
| Předmět: |
lcsh:GE1-350
020301 aerospace & aeronautics Engineering Spacecraft Ground business.industry Mechanical engineering 02 engineering and technology Anode voltage 7. Clean energy 01 natural sciences Cathode Hall effect thruster Cost savings law.invention 0203 mechanical engineering 13. Climate action law 0103 physical sciences business 010303 astronomy & astrophysics Galvanic isolation lcsh:Environmental sciences |
| Zdroj: | E3S Web of Conferences E3S Web of Conferences, Vol 16, p 15002 (2017) |
| ISSN: | 2267-1242 |
| DOI: | 10.1051/e3sconf/20171615002 |
| Popis: | In order to maximize system mass and cost savings, a Hall Effect Thruster Direct Drive Approach shall ideally get away with the need to provide galvanic isolation for the Anode voltage. In this respect, we present some experimental data aiming at characterising the implications of a direct connection between the HET Cathode Return Potential and the Spacecraft Ground. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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