Liquid metal ion thruster array

A Liquid Metal Ion Thruster (LMIT) has a substrate having a plurality of pedestals, one end of the pedestal attached to the substrate, and the opposing end of the pedestal having a tip, the pedestals having grooves and the substrate also having grooves coupled to each other and to a source of liquid...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Krishnan, Mahadevan, Wilson, Kristi, Champagne, Kelan, Wright, Jason D, Gerhan, Andrew N
Format: Patent
Sprache:eng
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator Krishnan, Mahadevan
Wilson, Kristi
Champagne, Kelan
Wright, Jason D
Gerhan, Andrew N
description A Liquid Metal Ion Thruster (LMIT) has a substrate having a plurality of pedestals, one end of the pedestal attached to the substrate, and the opposing end of the pedestal having a tip, the pedestals having grooves and the substrate also having grooves coupled to each other and to a source of liquid metal. An extractor electrode positioned parallel to the substrate and above the pedestal tips provides an electrostatic extraction field sufficient to accelerate ions from the tips of the pedestals through the extractor electrode. A series of focusing electrodes with matching apertures provides a flow of substantially parallel ion trajectories, and an optional negative ion source provides a charge neutralization to prevent space charge spreading of the exiting accelerated ions. The assembly is suitable for providing thrust for a satellite while maintaining high operating efficiencies.
format Patent
fullrecord <record><control><sourceid>uspatents_EFH</sourceid><recordid>TN_cdi_uspatents_grants_07827779</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>07827779</sourcerecordid><originalsourceid>FETCH-uspatents_grants_078277793</originalsourceid><addsrcrecordid>eNrjZJD3ySwszUxRyE0tScxRyMzPUyjJKCotLkktUkgsKkqs5GFgTUvMKU7lhdLcDApuriHOHrqlxQWJJal5JcXx6UWJIMrA3MLI3Nzc0pgIJQAN2yXz</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Liquid metal ion thruster array</title><source>USPTO Issued Patents</source><creator>Krishnan, Mahadevan ; Wilson, Kristi ; Champagne, Kelan ; Wright, Jason D ; Gerhan, Andrew N</creator><creatorcontrib>Krishnan, Mahadevan ; Wilson, Kristi ; Champagne, Kelan ; Wright, Jason D ; Gerhan, Andrew N ; Alameda Applied Sciences Corp</creatorcontrib><description>A Liquid Metal Ion Thruster (LMIT) has a substrate having a plurality of pedestals, one end of the pedestal attached to the substrate, and the opposing end of the pedestal having a tip, the pedestals having grooves and the substrate also having grooves coupled to each other and to a source of liquid metal. An extractor electrode positioned parallel to the substrate and above the pedestal tips provides an electrostatic extraction field sufficient to accelerate ions from the tips of the pedestals through the extractor electrode. A series of focusing electrodes with matching apertures provides a flow of substantially parallel ion trajectories, and an optional negative ion source provides a charge neutralization to prevent space charge spreading of the exiting accelerated ions. The assembly is suitable for providing thrust for a satellite while maintaining high operating efficiencies.</description><language>eng</language><creationdate>2010</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7827779$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,780,802,885,64037</link.rule.ids><linktorsrc>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7827779$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Krishnan, Mahadevan</creatorcontrib><creatorcontrib>Wilson, Kristi</creatorcontrib><creatorcontrib>Champagne, Kelan</creatorcontrib><creatorcontrib>Wright, Jason D</creatorcontrib><creatorcontrib>Gerhan, Andrew N</creatorcontrib><creatorcontrib>Alameda Applied Sciences Corp</creatorcontrib><title>Liquid metal ion thruster array</title><description>A Liquid Metal Ion Thruster (LMIT) has a substrate having a plurality of pedestals, one end of the pedestal attached to the substrate, and the opposing end of the pedestal having a tip, the pedestals having grooves and the substrate also having grooves coupled to each other and to a source of liquid metal. An extractor electrode positioned parallel to the substrate and above the pedestal tips provides an electrostatic extraction field sufficient to accelerate ions from the tips of the pedestals through the extractor electrode. A series of focusing electrodes with matching apertures provides a flow of substantially parallel ion trajectories, and an optional negative ion source provides a charge neutralization to prevent space charge spreading of the exiting accelerated ions. The assembly is suitable for providing thrust for a satellite while maintaining high operating efficiencies.</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2010</creationdate><recordtype>patent</recordtype><sourceid>EFH</sourceid><recordid>eNrjZJD3ySwszUxRyE0tScxRyMzPUyjJKCotLkktUkgsKkqs5GFgTUvMKU7lhdLcDApuriHOHrqlxQWJJal5JcXx6UWJIMrA3MLI3Nzc0pgIJQAN2yXz</recordid><startdate>20101109</startdate><enddate>20101109</enddate><creator>Krishnan, Mahadevan</creator><creator>Wilson, Kristi</creator><creator>Champagne, Kelan</creator><creator>Wright, Jason D</creator><creator>Gerhan, Andrew N</creator><scope>EFH</scope></search><sort><creationdate>20101109</creationdate><title>Liquid metal ion thruster array</title><author>Krishnan, Mahadevan ; Wilson, Kristi ; Champagne, Kelan ; Wright, Jason D ; Gerhan, Andrew N</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_grants_078277793</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2010</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Krishnan, Mahadevan</creatorcontrib><creatorcontrib>Wilson, Kristi</creatorcontrib><creatorcontrib>Champagne, Kelan</creatorcontrib><creatorcontrib>Wright, Jason D</creatorcontrib><creatorcontrib>Gerhan, Andrew N</creatorcontrib><creatorcontrib>Alameda Applied Sciences Corp</creatorcontrib><collection>USPTO Issued Patents</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Krishnan, Mahadevan</au><au>Wilson, Kristi</au><au>Champagne, Kelan</au><au>Wright, Jason D</au><au>Gerhan, Andrew N</au><aucorp>Alameda Applied Sciences Corp</aucorp><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Liquid metal ion thruster array</title><date>2010-11-09</date><risdate>2010</risdate><abstract>A Liquid Metal Ion Thruster (LMIT) has a substrate having a plurality of pedestals, one end of the pedestal attached to the substrate, and the opposing end of the pedestal having a tip, the pedestals having grooves and the substrate also having grooves coupled to each other and to a source of liquid metal. An extractor electrode positioned parallel to the substrate and above the pedestal tips provides an electrostatic extraction field sufficient to accelerate ions from the tips of the pedestals through the extractor electrode. A series of focusing electrodes with matching apertures provides a flow of substantially parallel ion trajectories, and an optional negative ion source provides a charge neutralization to prevent space charge spreading of the exiting accelerated ions. The assembly is suitable for providing thrust for a satellite while maintaining high operating efficiencies.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_uspatents_grants_07827779
source USPTO Issued Patents
title Liquid metal ion thruster array
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-09T21%3A55%3A24IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-uspatents_EFH&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Krishnan,%20Mahadevan&rft.aucorp=Alameda%20Applied%20Sciences%20Corp&rft.date=2010-11-09&rft_id=info:doi/&rft_dat=%3Cuspatents_EFH%3E07827779%3C/uspatents_EFH%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true