Contribution of electrostatic forces in ion propulsion for application in unmanned aerial vehicles
Electric Propulsion is prominently used in several kinds of unmanned aerial vehicles (UAV), in which propeller based propulsion system is usually used to propel the drone. This paper presents a study on role of electrostatic forces due to ionization for application in unmanned aerial vehicles. The d...
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description | Electric Propulsion is prominently used in several kinds of unmanned aerial vehicles (UAV), in which propeller based propulsion system is usually used to propel the drone. This paper presents a study on role of electrostatic forces due to ionization for application in unmanned aerial vehicles. The different geometries of electrodes in ion thrusters and contribution of electrostatic forces to the ion thrust of the drone are studied in this article. The study shows that the electrode geometry optimization could be influential for thrust augmentation in ion propelled UAVs. |
doi_str_mv | 10.1063/5.0216647 |
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The study shows that the electrode geometry optimization could be influential for thrust augmentation in ion propelled UAVs.</description><subject>Electric propulsion</subject><subject>Electrodes</subject><subject>Ion propulsion</subject><subject>Ion thrusters</subject><subject>Propulsion systems</subject><subject>Thrust augmentation</subject><subject>Unmanned aerial vehicles</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2024</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNotkElLBDEQhYMoOI4e_AcBb0KP2Ts5yuAGA17m4C2ks2CGnk6bpAX_vT3LqYp6X1U9HgD3GK0wEvSJrxDBQrD2Aiww57hpBRaXYIGQYg1h9Osa3JSyQ4iotpUL0K3TUHPsphrTAFOAvve25lSqqdHCkLL1BcYBHuQxp3Hqy6GdBWjGsY_WHDdnYhr2Zhi8g8bnaHr467-j7X25BVfB9MXfnesSbF9ftuv3ZvP59rF-3jSjoG0TODWGsi50pg1EGOGtooR5ZqUKyhHiHJFSMqeIDCY4jOeBsxwxg0PXSroED6ezs8ufyZeqd2nKw_xRUyQURRJzNVOPJ6rYWI_W9Zjj3uQ_jZE-RKi5PkdI_wFPl2Vy</recordid><startdate>20240618</startdate><enddate>20240618</enddate><creator>Rushikesh, Patil</creator><creator>Jain, Pulkit</creator><creator>Gill, Harjot Singh</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20240618</creationdate><title>Contribution of electrostatic forces in ion propulsion for application in unmanned aerial vehicles</title><author>Rushikesh, Patil ; Jain, Pulkit ; Gill, Harjot Singh</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p637-f53aa34bfba7f26a6ec9324e4c89f9d22dd28884d928fafd11dd2dc504a1fb783</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Electric propulsion</topic><topic>Electrodes</topic><topic>Ion propulsion</topic><topic>Ion thrusters</topic><topic>Propulsion systems</topic><topic>Thrust augmentation</topic><topic>Unmanned aerial vehicles</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Rushikesh, Patil</creatorcontrib><creatorcontrib>Jain, Pulkit</creatorcontrib><creatorcontrib>Gill, Harjot Singh</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Rushikesh, Patil</au><au>Jain, Pulkit</au><au>Gill, Harjot Singh</au><au>P, Thangaraj</au><au>H, Shankar</au><au>K, Mohana Sundaram</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Contribution of electrostatic forces in ion propulsion for application in unmanned aerial vehicles</atitle><btitle>AIP conference proceedings</btitle><date>2024-06-18</date><risdate>2024</risdate><volume>3122</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>Electric Propulsion is prominently used in several kinds of unmanned aerial vehicles (UAV), in which propeller based propulsion system is usually used to propel the drone. This paper presents a study on role of electrostatic forces due to ionization for application in unmanned aerial vehicles. The different geometries of electrodes in ion thrusters and contribution of electrostatic forces to the ion thrust of the drone are studied in this article. The study shows that the electrode geometry optimization could be influential for thrust augmentation in ion propelled UAVs.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0216647</doi><tpages>9</tpages></addata></record> |
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subjects | Electric propulsion Electrodes Ion propulsion Ion thrusters Propulsion systems Thrust augmentation Unmanned aerial vehicles |
title | Contribution of electrostatic forces in ion propulsion for application in unmanned aerial vehicles |
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