Investigation of promising ceramic materials in discharge chambers of stationary plasma thrusters
The characteristics of the insulator wear process in the discharge chamber of a stationary plasma thruster (SPT) are analyzed. The results of studying the erosion resistance to ionic spraying of different ceramic compositions are presented. It is shown experimentally that the integral characteristic...
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Veröffentlicht in: | Russian aeronautics 2008-12, Vol.51 (4), p.382-387 |
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creator | Khartov, S. A. Shkarban, I. I. |
description | The characteristics of the insulator wear process in the discharge chamber of a stationary plasma thruster (SPT) are analyzed. The results of studying the erosion resistance to ionic spraying of different ceramic compositions are presented. It is shown experimentally that the integral characteristics (the value of thrust and thrust efficiency) as well as the SPT lifetime can be improved in changing from the conventional hot-pressed boron silicate (BN + SiO
2
) ceramics to the BN + Si
3
N
4
ceramic compositions. |
doi_str_mv | 10.3103/S1068799808040065 |
format | Article |
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2
) ceramics to the BN + Si
3
N
4
ceramic compositions.</description><identifier>ISSN: 1068-7998</identifier><identifier>EISSN: 1934-7901</identifier><identifier>DOI: 10.3103/S1068799808040065</identifier><language>eng</language><publisher>Heidelberg: Allerton Press, Inc</publisher><subject>Aero- and Gas-Dynamics of Flight Vehicles and Their Engines ; Automotive Engineering ; Boron nitride ; Ceramics ; Chambers ; Discharge ; Engineering ; Insulators ; Silicates ; Stationary plasma thrusters ; Thrust</subject><ispartof>Russian aeronautics, 2008-12, Vol.51 (4), p.382-387</ispartof><rights>Allerton Press, Inc. 2008</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c2625-d4c660115ae8b4e5c4e2f53cce998ecb00a4032e2740d5517f85698c50cb3fb03</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.3103/S1068799808040065$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.3103/S1068799808040065$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,780,784,27924,27925,41488,42557,51319</link.rule.ids></links><search><creatorcontrib>Khartov, S. A.</creatorcontrib><creatorcontrib>Shkarban, I. I.</creatorcontrib><title>Investigation of promising ceramic materials in discharge chambers of stationary plasma thrusters</title><title>Russian aeronautics</title><addtitle>Russ. Aeronaut</addtitle><description>The characteristics of the insulator wear process in the discharge chamber of a stationary plasma thruster (SPT) are analyzed. The results of studying the erosion resistance to ionic spraying of different ceramic compositions are presented. It is shown experimentally that the integral characteristics (the value of thrust and thrust efficiency) as well as the SPT lifetime can be improved in changing from the conventional hot-pressed boron silicate (BN + SiO
2
) ceramics to the BN + Si
3
N
4
ceramic compositions.</description><subject>Aero- and Gas-Dynamics of Flight Vehicles and Their Engines</subject><subject>Automotive Engineering</subject><subject>Boron nitride</subject><subject>Ceramics</subject><subject>Chambers</subject><subject>Discharge</subject><subject>Engineering</subject><subject>Insulators</subject><subject>Silicates</subject><subject>Stationary plasma thrusters</subject><subject>Thrust</subject><issn>1068-7998</issn><issn>1934-7901</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2008</creationdate><recordtype>article</recordtype><recordid>eNp1kEtLxDAUhYMoOD5-gLvgxlX15tUmSxl8DAy4UNclzdx2MkzbMWkF_72pIwiKq3vhnu9wzyHkgsG1YCBunhnkujBGgwYJkKsDMmNGyKwwwA7Tns7ZdD8mJzFuAFTOJZ8Ru-jeMQ6-sYPvO9rXdBf61kffNdRhsK13tLUDBm-3kfqOrnx0axsapGm0FYY4QXH44m34oLutja2lwzqMMXHxjBzVicXz73lKXu_vXuaP2fLpYTG_XWaO51xlK-nyHBhTFnUlUTmJvFbCOUxPo6sArATBkRcSVkqxotYqN9opcJWoKxCn5GrvmwK8jSlTmWI43G5th_0YS8OM4YXgk_Lyl3LTj6FLz5Vai2QNnCcR24tc6GMMWJe74NsUsGRQTpWXfypPDN8zMWm7BsOP8f_QJ-dEg8Q</recordid><startdate>20081201</startdate><enddate>20081201</enddate><creator>Khartov, S. A.</creator><creator>Shkarban, I. I.</creator><general>Allerton Press, Inc</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>7QQ</scope><scope>JG9</scope></search><sort><creationdate>20081201</creationdate><title>Investigation of promising ceramic materials in discharge chambers of stationary plasma thrusters</title><author>Khartov, S. A. ; Shkarban, I. I.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2625-d4c660115ae8b4e5c4e2f53cce998ecb00a4032e2740d5517f85698c50cb3fb03</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2008</creationdate><topic>Aero- and Gas-Dynamics of Flight Vehicles and Their Engines</topic><topic>Automotive Engineering</topic><topic>Boron nitride</topic><topic>Ceramics</topic><topic>Chambers</topic><topic>Discharge</topic><topic>Engineering</topic><topic>Insulators</topic><topic>Silicates</topic><topic>Stationary plasma thrusters</topic><topic>Thrust</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Khartov, S. A.</creatorcontrib><creatorcontrib>Shkarban, I. I.</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Ceramic Abstracts</collection><collection>Materials Research Database</collection><jtitle>Russian aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Khartov, S. A.</au><au>Shkarban, I. I.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Investigation of promising ceramic materials in discharge chambers of stationary plasma thrusters</atitle><jtitle>Russian aeronautics</jtitle><stitle>Russ. Aeronaut</stitle><date>2008-12-01</date><risdate>2008</risdate><volume>51</volume><issue>4</issue><spage>382</spage><epage>387</epage><pages>382-387</pages><issn>1068-7998</issn><eissn>1934-7901</eissn><abstract>The characteristics of the insulator wear process in the discharge chamber of a stationary plasma thruster (SPT) are analyzed. The results of studying the erosion resistance to ionic spraying of different ceramic compositions are presented. It is shown experimentally that the integral characteristics (the value of thrust and thrust efficiency) as well as the SPT lifetime can be improved in changing from the conventional hot-pressed boron silicate (BN + SiO
2
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3
N
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subjects | Aero- and Gas-Dynamics of Flight Vehicles and Their Engines Automotive Engineering Boron nitride Ceramics Chambers Discharge Engineering Insulators Silicates Stationary plasma thrusters Thrust |
title | Investigation of promising ceramic materials in discharge chambers of stationary plasma thrusters |
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