Modeling of Plasma Flow Around SMART-1 Spacecraft
SMART-1 is the first European spacecraft that uses electric propulsion as the main propulsion system. The thruster characteristics and plasma measurements performed during SMART-1 mission lay a good foundation for understanding spacecraft/plasma interactions. This paper discusses the applications an...
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| Veröffentlicht in: | IEEE transactions on plasma science 2006-10, Vol.34 (5), p.2166-2175 |
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| creator | Markelov, G. Gengembre, E. |
| description | SMART-1 is the first European spacecraft that uses electric propulsion as the main propulsion system. The thruster characteristics and plasma measurements performed during SMART-1 mission lay a good foundation for understanding spacecraft/plasma interactions. This paper discusses the applications and modifications of spacecraft plasma interaction system software, which originally was developed to simulate an interaction of the space plasma with the spacecraft-surface materials and to compute a plasma-induced charging. The particle-in-cell and Monte Carlo collision (PIC-MCC) method and a simplified and fast approach that tracks only slow ion motion are implemented to model the plasma flow around the spacecraft with electric propulsion. The simplified approach consists of a consecutive application of a direct simulation MC (DSMC)-based software for neutral flow, axisymmetric PIC-MCC for plume flow, and three-dimensional (3-D) PIC software for plasma flow around the spacecraft. Three-dimensional computations are performed to analyze the effects of single- and double-charged Xenon ions, constant and spatially variable electron temperature, an application of quasi-neutral assumption or Poisson solver, and low Earth orbit environment on plasma flow around SMART-1. It was shown that a spatially variable electron temperature has the most significant effect on the plasma-flow properties |
| doi_str_mv | 10.1109/TPS.2006.879098 |
| format | Article |
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The thruster characteristics and plasma measurements performed during SMART-1 mission lay a good foundation for understanding spacecraft/plasma interactions. This paper discusses the applications and modifications of spacecraft plasma interaction system software, which originally was developed to simulate an interaction of the space plasma with the spacecraft-surface materials and to compute a plasma-induced charging. The particle-in-cell and Monte Carlo collision (PIC-MCC) method and a simplified and fast approach that tracks only slow ion motion are implemented to model the plasma flow around the spacecraft with electric propulsion. The simplified approach consists of a consecutive application of a direct simulation MC (DSMC)-based software for neutral flow, axisymmetric PIC-MCC for plume flow, and three-dimensional (3-D) PIC software for plasma flow around the spacecraft. Three-dimensional computations are performed to analyze the effects of single- and double-charged Xenon ions, constant and spatially variable electron temperature, an application of quasi-neutral assumption or Poisson solver, and low Earth orbit environment on plasma flow around SMART-1. 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(IEEE) Oct 2006</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c350t-4c8215f2168cae3c603f2344ba8d1085f86772a0ce567c5b9398f1a757f3a0493</citedby><cites>FETCH-LOGICAL-c350t-4c8215f2168cae3c603f2344ba8d1085f86772a0ce567c5b9398f1a757f3a0493</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/1710094$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,314,780,784,789,790,796,23930,23931,25140,27924,27925,54758</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/1710094$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=18251952$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Markelov, G.</creatorcontrib><creatorcontrib>Gengembre, E.</creatorcontrib><title>Modeling of Plasma Flow Around SMART-1 Spacecraft</title><title>IEEE transactions on plasma science</title><addtitle>TPS</addtitle><description>SMART-1 is the first European spacecraft that uses electric propulsion as the main propulsion system. The thruster characteristics and plasma measurements performed during SMART-1 mission lay a good foundation for understanding spacecraft/plasma interactions. This paper discusses the applications and modifications of spacecraft plasma interaction system software, which originally was developed to simulate an interaction of the space plasma with the spacecraft-surface materials and to compute a plasma-induced charging. The particle-in-cell and Monte Carlo collision (PIC-MCC) method and a simplified and fast approach that tracks only slow ion motion are implemented to model the plasma flow around the spacecraft with electric propulsion. The simplified approach consists of a consecutive application of a direct simulation MC (DSMC)-based software for neutral flow, axisymmetric PIC-MCC for plume flow, and three-dimensional (3-D) PIC software for plasma flow around the spacecraft. Three-dimensional computations are performed to analyze the effects of single- and double-charged Xenon ions, constant and spatially variable electron temperature, an application of quasi-neutral assumption or Poisson solver, and low Earth orbit environment on plasma flow around SMART-1. It was shown that a spatially variable electron temperature has the most significant effect on the plasma-flow properties</description><subject>Aircraft manufacture</subject><subject>Application software</subject><subject>Charged particles</subject><subject>Computer programs</subject><subject>Computer simulation</subject><subject>Electric power</subject><subject>Electric propulsion</subject><subject>Electron temperature</subject><subject>Exact sciences and technology</subject><subject>Ion and plasma propulsion</subject><subject>Laboratoty studies of space- and astrophysical plasmas</subject><subject>modeling</subject><subject>Monte Carlo methods</subject><subject>Monte Carlo simulation</subject><subject>Particle-in-cell method</subject><subject>Physics</subject><subject>Physics of gases, plasmas and electric discharges</subject><subject>Physics of plasmas and electric discharges</subject><subject>Plasma</subject><subject>Plasma applications</subject><subject>Plasma devices</subject><subject>plasma flow</subject><subject>Plasma interactions</subject><subject>Plasma materials processing</subject><subject>Plasma measurements</subject><subject>Plasma properties</subject><subject>Plasma simulation</subject><subject>Plasma temperature</subject><subject>Propulsion</subject><subject>Software</subject><subject>Space vehicles</subject><subject>Spacecraft</subject><issn>0093-3813</issn><issn>1939-9375</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2006</creationdate><recordtype>article</recordtype><sourceid>RIE</sourceid><recordid>eNpdkEFLAzEQhYMoWKtnD14WQTxtO5NsNsmxFKtCi8XWc0jTRLZsd2vSRfz3prQgeJrDfO_x-Ai5RRggghou54sBBSgHUihQ8oz0UDGVKyb4OekBKJYzieySXMW4AcCCA-0RnLVrV1fNZ9b6bF6buDXZpG6_s1Fou2adLWaj92WO2WJnrLPB-P01ufCmju7mdPvkY_K0HL_k07fn1_FomlvGYZ8XVlLknmIprXHMlsA8ZUWxMnKNILmXpRDUgHW8FJav0lbp0QguPDNQKNYnj8feXWi_Ohf3eltF6-raNK7topZSMcmE5Im8_0du2i40aZxGxVEUQmGChkfIhjbG4LzehWprwo9G0AeBOgnUB4H6KDAlHk61JlpT-2AaW8W_mKQ81dPE3R25yjn39xaYnBfsF0BcdRM</recordid><startdate>20061001</startdate><enddate>20061001</enddate><creator>Markelov, G.</creator><creator>Gengembre, E.</creator><general>IEEE</general><general>Institute of Electrical and Electronics Engineers</general><general>The Institute of Electrical and Electronics Engineers, Inc. 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The thruster characteristics and plasma measurements performed during SMART-1 mission lay a good foundation for understanding spacecraft/plasma interactions. This paper discusses the applications and modifications of spacecraft plasma interaction system software, which originally was developed to simulate an interaction of the space plasma with the spacecraft-surface materials and to compute a plasma-induced charging. The particle-in-cell and Monte Carlo collision (PIC-MCC) method and a simplified and fast approach that tracks only slow ion motion are implemented to model the plasma flow around the spacecraft with electric propulsion. The simplified approach consists of a consecutive application of a direct simulation MC (DSMC)-based software for neutral flow, axisymmetric PIC-MCC for plume flow, and three-dimensional (3-D) PIC software for plasma flow around the spacecraft. Three-dimensional computations are performed to analyze the effects of single- and double-charged Xenon ions, constant and spatially variable electron temperature, an application of quasi-neutral assumption or Poisson solver, and low Earth orbit environment on plasma flow around SMART-1. It was shown that a spatially variable electron temperature has the most significant effect on the plasma-flow properties</abstract><cop>New York, NY</cop><pub>IEEE</pub><doi>10.1109/TPS.2006.879098</doi><tpages>10</tpages></addata></record> |
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| subjects | Aircraft manufacture Application software Charged particles Computer programs Computer simulation Electric power Electric propulsion Electron temperature Exact sciences and technology Ion and plasma propulsion Laboratoty studies of space- and astrophysical plasmas modeling Monte Carlo methods Monte Carlo simulation Particle-in-cell method Physics Physics of gases, plasmas and electric discharges Physics of plasmas and electric discharges Plasma Plasma applications Plasma devices plasma flow Plasma interactions Plasma materials processing Plasma measurements Plasma properties Plasma simulation Plasma temperature Propulsion Software Space vehicles Spacecraft |
| title | Modeling of Plasma Flow Around SMART-1 Spacecraft |
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