Modelling studies of charged particle interactions for a space application
An electron emitter neutraliser to prevent spacecraft charging from the use of positive ion thrusters is under development at the Rutherford Appleton Laboratory. A particle-in-cell code, KARAT, has been used to simulate laboratory experiments, Laboratory test results have been successfully obtained...
| 主要な著者: | , |
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| フォーマット: | Journal article |
| 言語: | English |
| 出版事項: |
2004
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| _version_ | 1826289357954220032 |
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| author | Aplin, K Tarakanov, V |
| author_facet | Aplin, K Tarakanov, V |
| author_sort | Aplin, K |
| collection | OXFORD |
| description | An electron emitter neutraliser to prevent spacecraft charging from the use of positive ion thrusters is under development at the Rutherford Appleton Laboratory. A particle-in-cell code, KARAT, has been used to simulate laboratory experiments, Laboratory test results have been successfully obtained with simulations, for model verification. Neutraliser-ion thruster interactions in space have also been modelled. An ion-propelled spacecraft rapidly charges to kilovolt potentials, which can be dissipated by an electron-emitting neutraliser. The effect of background particle concentrations on neutralisation has also been studied. |
| first_indexed | 2024-03-07T02:27:39Z |
| format | Journal article |
| id | oxford-uuid:a62c4dfc-b36c-43c0-95f5-3f8a03fd2bca |
| institution | University of Oxford |
| language | English |
| last_indexed | 2024-03-07T02:27:39Z |
| publishDate | 2004 |
| record_format | dspace |
| spelling | oxford-uuid:a62c4dfc-b36c-43c0-95f5-3f8a03fd2bca2022-03-27T02:45:18ZModelling studies of charged particle interactions for a space applicationJournal articlehttp://purl.org/coar/resource_type/c_dcae04bcuuid:a62c4dfc-b36c-43c0-95f5-3f8a03fd2bcaEnglishSymplectic Elements at Oxford2004Aplin, KTarakanov, VAn electron emitter neutraliser to prevent spacecraft charging from the use of positive ion thrusters is under development at the Rutherford Appleton Laboratory. A particle-in-cell code, KARAT, has been used to simulate laboratory experiments, Laboratory test results have been successfully obtained with simulations, for model verification. Neutraliser-ion thruster interactions in space have also been modelled. An ion-propelled spacecraft rapidly charges to kilovolt potentials, which can be dissipated by an electron-emitting neutraliser. The effect of background particle concentrations on neutralisation has also been studied. |
| spellingShingle | Aplin, K Tarakanov, V Modelling studies of charged particle interactions for a space application |
| title | Modelling studies of charged particle interactions for a space application |
| title_full | Modelling studies of charged particle interactions for a space application |
| title_fullStr | Modelling studies of charged particle interactions for a space application |
| title_full_unstemmed | Modelling studies of charged particle interactions for a space application |
| title_short | Modelling studies of charged particle interactions for a space application |
| title_sort | modelling studies of charged particle interactions for a space application |
| work_keys_str_mv | AT aplink modellingstudiesofchargedparticleinteractionsforaspaceapplication AT tarakanovv modellingstudiesofchargedparticleinteractionsforaspaceapplication |