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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Rushikesh, Patil, Jain, Pulkit, Gill, Harjot Singh
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue 1
container_start_page
container_title
container_volume 3122
creator Rushikesh, Patil
Jain, Pulkit
Gill, Harjot Singh
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
format Conference Proceeding
fullrecord <record><control><sourceid>proquest_scita</sourceid><recordid>TN_cdi_proquest_journals_3069308159</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>3069308159</sourcerecordid><originalsourceid>FETCH-LOGICAL-p637-f53aa34bfba7f26a6ec9324e4c89f9d22dd28884d928fafd11dd2dc504a1fb783</originalsourceid><addsrcrecordid>eNotkElLBDEQhYMoOI4e_AcBb0KP2Ts5yuAGA17m4C2ks2CGnk6bpAX_vT3LqYp6X1U9HgD3GK0wEvSJrxDBQrD2Aiww57hpBRaXYIGQYg1h9Osa3JSyQ4iotpUL0K3TUHPsphrTAFOAvve25lSqqdHCkLL1BcYBHuQxp3Hqy6GdBWjGsY_WHDdnYhr2Zhi8g8bnaHr467-j7X25BVfB9MXfnesSbF9ftuv3ZvP59rF-3jSjoG0TODWGsi50pg1EGOGtooR5ZqUKyhHiHJFSMqeIDCY4jOeBsxwxg0PXSroED6ezs8ufyZeqd2nKw_xRUyQURRJzNVOPJ6rYWI_W9Zjj3uQ_jZE-RKi5PkdI_wFPl2Vy</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype><pqid>3069308159</pqid></control><display><type>conference_proceeding</type><title>Contribution of electrostatic forces in ion propulsion for application in unmanned aerial vehicles</title><source>AIP Journals Complete</source><creator>Rushikesh, Patil ; Jain, Pulkit ; Gill, Harjot Singh</creator><contributor>P, Thangaraj ; H, Shankar ; K, Mohana Sundaram</contributor><creatorcontrib>Rushikesh, Patil ; Jain, Pulkit ; Gill, Harjot Singh ; P, Thangaraj ; H, Shankar ; K, Mohana Sundaram</creatorcontrib><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.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/5.0216647</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Electric propulsion ; Electrodes ; Ion propulsion ; Ion thrusters ; Propulsion systems ; Thrust augmentation ; Unmanned aerial vehicles</subject><ispartof>AIP conference proceedings, 2024, Vol.3122 (1)</ispartof><rights>Author(s)</rights><rights>2024 Author(s). Published under an exclusive license by AIP Publishing.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://pubs.aip.org/acp/article-lookup/doi/10.1063/5.0216647$$EHTML$$P50$$Gscitation$$H</linktohtml><link.rule.ids>309,310,314,778,782,787,788,792,4500,23919,23920,25129,27913,27914,76143</link.rule.ids></links><search><contributor>P, Thangaraj</contributor><contributor>H, Shankar</contributor><contributor>K, Mohana Sundaram</contributor><creatorcontrib>Rushikesh, Patil</creatorcontrib><creatorcontrib>Jain, Pulkit</creatorcontrib><creatorcontrib>Gill, Harjot Singh</creatorcontrib><title>Contribution of electrostatic forces in ion propulsion for application in unmanned aerial vehicles</title><title>AIP conference proceedings</title><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.</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>
fulltext fulltext
identifier ISSN: 0094-243X
ispartof AIP conference proceedings, 2024, Vol.3122 (1)
issn 0094-243X
1551-7616
language eng
recordid cdi_proquest_journals_3069308159
source AIP Journals Complete
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
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-15T09%3A57%3A16IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_scita&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Contribution%20of%20electrostatic%20forces%20in%20ion%20propulsion%20for%20application%20in%20unmanned%20aerial%20vehicles&rft.btitle=AIP%20conference%20proceedings&rft.au=Rushikesh,%20Patil&rft.date=2024-06-18&rft.volume=3122&rft.issue=1&rft.issn=0094-243X&rft.eissn=1551-7616&rft.coden=APCPCS&rft_id=info:doi/10.1063/5.0216647&rft_dat=%3Cproquest_scita%3E3069308159%3C/proquest_scita%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=3069308159&rft_id=info:pmid/&rfr_iscdi=true