Meteoroid and technogenic particle impact on spacecraft solar panels
This paper presents calculated models and the results of estimates of meteoroid and technogenic particle impact on spacecraft solar panels. It is shown that optical losses resulting from the formation of microcraters on the surface of protective glasses of semiconductor photoconverters (PC) are negl...
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| Veröffentlicht in: | Cosmic research 2016-09, Vol.54 (5), p.366-374 |
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| creator | Nadiradze, A. B. Kalaev, M. P. Semkin, N. D. |
| description | This paper presents calculated models and the results of estimates of meteoroid and technogenic particle impact on spacecraft solar panels. It is shown that optical losses resulting from the formation of microcraters on the surface of protective glasses of semiconductor photoconverters (PC) are negligible (less than 0.01%). Significantly greater losses can occur as a result of shunting the PC
p–n
junction. In high and medium orbits, these losses are 0.1–0.2%/year for the glass thickness of 150 μm and the area of one PC of 30 cm
2
. Decreasing the glass thickness up to 100 μm can lead to increasing power losses up to 0.6%/year. |
| doi_str_mv | 10.1134/S001095251605004X |
| format | Article |
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p–n
junction. In high and medium orbits, these losses are 0.1–0.2%/year for the glass thickness of 150 μm and the area of one PC of 30 cm
2
. Decreasing the glass thickness up to 100 μm can lead to increasing power losses up to 0.6%/year.</description><identifier>ISSN: 0010-9525</identifier><identifier>EISSN: 1608-3075</identifier><identifier>DOI: 10.1134/S001095251605004X</identifier><language>eng</language><publisher>Moscow: Pleiades Publishing</publisher><subject>Astronomy ; Astrophysics and Astroparticles ; Astrophysics and Cosmology ; Glass ; Meteoroids ; Meteors & meteorites ; Orbits ; P-n junctions ; Panels ; Particle impact ; Photovoltaics ; Physics ; Physics and Astronomy ; Power loss ; Semiconductors ; Solar panels ; Space Exploration and Astronautics ; Space Sciences (including Extraterrestrial Physics ; Spacecraft</subject><ispartof>Cosmic research, 2016-09, Vol.54 (5), p.366-374</ispartof><rights>Pleiades Publishing, Ltd. 2016</rights><rights>Copyright Springer Science & Business Media 2016</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c382t-2a431ef2ab26e4eba6eed0ded1f9116e104f5a2c242b72da149f76abbd8424ea3</citedby><cites>FETCH-LOGICAL-c382t-2a431ef2ab26e4eba6eed0ded1f9116e104f5a2c242b72da149f76abbd8424ea3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1134/S001095251605004X$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1134/S001095251605004X$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,780,784,27924,27925,41488,42557,51319</link.rule.ids></links><search><creatorcontrib>Nadiradze, A. B.</creatorcontrib><creatorcontrib>Kalaev, M. P.</creatorcontrib><creatorcontrib>Semkin, N. D.</creatorcontrib><title>Meteoroid and technogenic particle impact on spacecraft solar panels</title><title>Cosmic research</title><addtitle>Cosmic Res</addtitle><description>This paper presents calculated models and the results of estimates of meteoroid and technogenic particle impact on spacecraft solar panels. It is shown that optical losses resulting from the formation of microcraters on the surface of protective glasses of semiconductor photoconverters (PC) are negligible (less than 0.01%). Significantly greater losses can occur as a result of shunting the PC
p–n
junction. In high and medium orbits, these losses are 0.1–0.2%/year for the glass thickness of 150 μm and the area of one PC of 30 cm
2
. Decreasing the glass thickness up to 100 μm can lead to increasing power losses up to 0.6%/year.</description><subject>Astronomy</subject><subject>Astrophysics and Astroparticles</subject><subject>Astrophysics and Cosmology</subject><subject>Glass</subject><subject>Meteoroids</subject><subject>Meteors & meteorites</subject><subject>Orbits</subject><subject>P-n junctions</subject><subject>Panels</subject><subject>Particle impact</subject><subject>Photovoltaics</subject><subject>Physics</subject><subject>Physics and Astronomy</subject><subject>Power loss</subject><subject>Semiconductors</subject><subject>Solar panels</subject><subject>Space Exploration and Astronautics</subject><subject>Space Sciences (including Extraterrestrial Physics</subject><subject>Spacecraft</subject><issn>0010-9525</issn><issn>1608-3075</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNqNkU9LxDAQxYMouK5-AG8FL16qM2matEfxP6x4UMFbSNPp2qXb1KR78NubsoKgCMLAPJjfe8wwjB0jnCFm4vwJAKHMeY4ScgDxusNmURZpBirfZbNpnE7zfXYQwgoASpXJGbt6oJGcd22dmL5ORrJvvVtS39pkMH5sbUdJux6MHRPXJyEKst40YxJcZ3xkeurCIdtrTBfo6KvP2cvN9fPlXbp4vL2_vFikNiv4mHIjMqSGm4pLElQZSVRDTTU2JaIkBNHkhlsueKV4bVCUjZKmqupCcEEmm7PTbe7g3fuGwqjXbbDUdXELtwkaC5GrUiip_oFyVWIWK6InP9CV2_g-HqI5SCGLMpcThVvKeheCp0YPvl0b_6ER9PQC_esF0cO3nhDZfkn-O_lv0ycDRoef</recordid><startdate>20160901</startdate><enddate>20160901</enddate><creator>Nadiradze, A. B.</creator><creator>Kalaev, M. P.</creator><creator>Semkin, N. D.</creator><general>Pleiades Publishing</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TG</scope><scope>8FD</scope><scope>H8D</scope><scope>KL.</scope><scope>L7M</scope></search><sort><creationdate>20160901</creationdate><title>Meteoroid and technogenic particle impact on spacecraft solar panels</title><author>Nadiradze, A. B. ; Kalaev, M. P. ; Semkin, N. D.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c382t-2a431ef2ab26e4eba6eed0ded1f9116e104f5a2c242b72da149f76abbd8424ea3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>Astronomy</topic><topic>Astrophysics and Astroparticles</topic><topic>Astrophysics and Cosmology</topic><topic>Glass</topic><topic>Meteoroids</topic><topic>Meteors & meteorites</topic><topic>Orbits</topic><topic>P-n junctions</topic><topic>Panels</topic><topic>Particle impact</topic><topic>Photovoltaics</topic><topic>Physics</topic><topic>Physics and Astronomy</topic><topic>Power loss</topic><topic>Semiconductors</topic><topic>Solar panels</topic><topic>Space Exploration and Astronautics</topic><topic>Space Sciences (including Extraterrestrial Physics</topic><topic>Spacecraft</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Nadiradze, A. B.</creatorcontrib><creatorcontrib>Kalaev, M. P.</creatorcontrib><creatorcontrib>Semkin, N. D.</creatorcontrib><collection>CrossRef</collection><collection>Meteorological & Geoastrophysical Abstracts</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Meteorological & Geoastrophysical Abstracts - Academic</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Cosmic research</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Nadiradze, A. B.</au><au>Kalaev, M. P.</au><au>Semkin, N. D.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Meteoroid and technogenic particle impact on spacecraft solar panels</atitle><jtitle>Cosmic research</jtitle><stitle>Cosmic Res</stitle><date>2016-09-01</date><risdate>2016</risdate><volume>54</volume><issue>5</issue><spage>366</spage><epage>374</epage><pages>366-374</pages><issn>0010-9525</issn><eissn>1608-3075</eissn><abstract>This paper presents calculated models and the results of estimates of meteoroid and technogenic particle impact on spacecraft solar panels. It is shown that optical losses resulting from the formation of microcraters on the surface of protective glasses of semiconductor photoconverters (PC) are negligible (less than 0.01%). Significantly greater losses can occur as a result of shunting the PC
p–n
junction. In high and medium orbits, these losses are 0.1–0.2%/year for the glass thickness of 150 μm and the area of one PC of 30 cm
2
. Decreasing the glass thickness up to 100 μm can lead to increasing power losses up to 0.6%/year.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.1134/S001095251605004X</doi><tpages>9</tpages></addata></record> |
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| ispartof | Cosmic research, 2016-09, Vol.54 (5), p.366-374 |
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| subjects | Astronomy Astrophysics and Astroparticles Astrophysics and Cosmology Glass Meteoroids Meteors & meteorites Orbits P-n junctions Panels Particle impact Photovoltaics Physics Physics and Astronomy Power loss Semiconductors Solar panels Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Spacecraft |
| title | Meteoroid and technogenic particle impact on spacecraft solar panels |
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