Performance of high-efficiency advanced triple-junction solar panels for the LILT Mission Dawn
NASA's Discovery Mission Dawn is designed to operate within the solar system's Asteroid belt, where the large distance from the sun creates a low-intensity, low-temperature (LILT) condition. To meet the mission power requirements under LILT conditions, very high-efficiency multijunction so...
Gespeichert in:
| Hauptverfasser: | , , , , , , , , , , |
|---|---|
| Format: | Tagungsbericht |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 621 |
|---|---|
| container_issue | |
| container_start_page | 618 |
| container_title | |
| container_volume | |
| creator | Fatemi, N.S. Sharma, S. Buitrago, O. Crisman, J. Sharps, P.R. Blok, R. Kroon, M. Jalink, Cees Harris, R. Stella, P. Distefano, S. |
| description | NASA's Discovery Mission Dawn is designed to operate within the solar system's Asteroid belt, where the large distance from the sun creates a low-intensity, low-temperature (LILT) condition. To meet the mission power requirements under LILT conditions, very high-efficiency multijunction solar cells were selected to power the spacecraft to be built by Orbital Sciences Corporation (OSC) under contract to JPL. Emcore's InGaP/InGaAs/Ge advanced triple-junction (ATJ) solar cells, exhibiting an average air mass zero (AM0) efficiency of greater than 27.6% (one-sun, 28/spl deg/C), were used to populate the solar panels. The two solar array wings, to be built by Dutch Space, with 5 large-area panels each (total area of 36.4 m/sup 2/) are projected to produce between 10.3 kWe and 1.3 kWe of end-of-life (EOL) power in the 1.0 to 3.0 AU range, respectively. The details of the solar panel design, testing and power analysis are presented. |
| doi_str_mv | 10.1109/PVSC.2005.1488207 |
| format | Conference Proceeding |
| fullrecord | <record><control><sourceid>ieee_6IE</sourceid><recordid>TN_cdi_ieee_primary_1488207</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>1488207</ieee_id><sourcerecordid>1488207</sourcerecordid><originalsourceid>FETCH-LOGICAL-i175t-62409d4d273792652450b10676a94a8e83534c76626b98f6ceb539935e0ab09a3</originalsourceid><addsrcrecordid>eNotUNtKw0AUXFDBUvMB4sv-QOrZ--6j1FshYsHqo2WTnJgtaRKyUenfm2KHgXmYYRiGkGsGC8bA3a4_3pYLDqAWTFrLwZyRxBkLE4U1YPg5mQHTkFph2CVJYtzBBKmEcWpGPtc4VN2w922BtKtoHb7qFKsqFAHb4kB9-XO0SjoOoW8w3X23xRi6lsau8QPtfYtNpFMDHWuk2Srb0JcQ4zFx73_bK3JR-SZictI5eX982Cyf0-z1abW8y9LAjBpTzSW4UpbcTKu4VlwqyBloo72T3qIVSsjCaM117mylC8yVcE4oBJ-D82JObv57AyJu-yHs_XDYnh4Rf_BhU4k</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Performance of high-efficiency advanced triple-junction solar panels for the LILT Mission Dawn</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Fatemi, N.S. ; Sharma, S. ; Buitrago, O. ; Crisman, J. ; Sharps, P.R. ; Blok, R. ; Kroon, M. ; Jalink, Cees ; Harris, R. ; Stella, P. ; Distefano, S.</creator><creatorcontrib>Fatemi, N.S. ; Sharma, S. ; Buitrago, O. ; Crisman, J. ; Sharps, P.R. ; Blok, R. ; Kroon, M. ; Jalink, Cees ; Harris, R. ; Stella, P. ; Distefano, S.</creatorcontrib><description>NASA's Discovery Mission Dawn is designed to operate within the solar system's Asteroid belt, where the large distance from the sun creates a low-intensity, low-temperature (LILT) condition. To meet the mission power requirements under LILT conditions, very high-efficiency multijunction solar cells were selected to power the spacecraft to be built by Orbital Sciences Corporation (OSC) under contract to JPL. Emcore's InGaP/InGaAs/Ge advanced triple-junction (ATJ) solar cells, exhibiting an average air mass zero (AM0) efficiency of greater than 27.6% (one-sun, 28/spl deg/C), were used to populate the solar panels. The two solar array wings, to be built by Dutch Space, with 5 large-area panels each (total area of 36.4 m/sup 2/) are projected to produce between 10.3 kWe and 1.3 kWe of end-of-life (EOL) power in the 1.0 to 3.0 AU range, respectively. The details of the solar panel design, testing and power analysis are presented.</description><identifier>ISSN: 0160-8371</identifier><identifier>ISBN: 9780780387072</identifier><identifier>ISBN: 0780387074</identifier><identifier>DOI: 10.1109/PVSC.2005.1488207</identifier><language>eng</language><publisher>IEEE</publisher><subject>Aircraft manufacture ; Belts ; Gold ; Manufacturing ; Photovoltaic cells ; Production ; Space technology ; Sun ; Temperature ; Testing</subject><ispartof>Conference Record of the Thirty-first IEEE Photovoltaic Specialists Conference, 2005, 2005, p.618-621</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/1488207$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,780,784,789,790,2058,4050,4051,27925,54920</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/1488207$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Fatemi, N.S.</creatorcontrib><creatorcontrib>Sharma, S.</creatorcontrib><creatorcontrib>Buitrago, O.</creatorcontrib><creatorcontrib>Crisman, J.</creatorcontrib><creatorcontrib>Sharps, P.R.</creatorcontrib><creatorcontrib>Blok, R.</creatorcontrib><creatorcontrib>Kroon, M.</creatorcontrib><creatorcontrib>Jalink, Cees</creatorcontrib><creatorcontrib>Harris, R.</creatorcontrib><creatorcontrib>Stella, P.</creatorcontrib><creatorcontrib>Distefano, S.</creatorcontrib><title>Performance of high-efficiency advanced triple-junction solar panels for the LILT Mission Dawn</title><title>Conference Record of the Thirty-first IEEE Photovoltaic Specialists Conference, 2005</title><addtitle>PVSC</addtitle><description>NASA's Discovery Mission Dawn is designed to operate within the solar system's Asteroid belt, where the large distance from the sun creates a low-intensity, low-temperature (LILT) condition. To meet the mission power requirements under LILT conditions, very high-efficiency multijunction solar cells were selected to power the spacecraft to be built by Orbital Sciences Corporation (OSC) under contract to JPL. Emcore's InGaP/InGaAs/Ge advanced triple-junction (ATJ) solar cells, exhibiting an average air mass zero (AM0) efficiency of greater than 27.6% (one-sun, 28/spl deg/C), were used to populate the solar panels. The two solar array wings, to be built by Dutch Space, with 5 large-area panels each (total area of 36.4 m/sup 2/) are projected to produce between 10.3 kWe and 1.3 kWe of end-of-life (EOL) power in the 1.0 to 3.0 AU range, respectively. The details of the solar panel design, testing and power analysis are presented.</description><subject>Aircraft manufacture</subject><subject>Belts</subject><subject>Gold</subject><subject>Manufacturing</subject><subject>Photovoltaic cells</subject><subject>Production</subject><subject>Space technology</subject><subject>Sun</subject><subject>Temperature</subject><subject>Testing</subject><issn>0160-8371</issn><isbn>9780780387072</isbn><isbn>0780387074</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2005</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNotUNtKw0AUXFDBUvMB4sv-QOrZ--6j1FshYsHqo2WTnJgtaRKyUenfm2KHgXmYYRiGkGsGC8bA3a4_3pYLDqAWTFrLwZyRxBkLE4U1YPg5mQHTkFph2CVJYtzBBKmEcWpGPtc4VN2w922BtKtoHb7qFKsqFAHb4kB9-XO0SjoOoW8w3X23xRi6lsau8QPtfYtNpFMDHWuk2Srb0JcQ4zFx73_bK3JR-SZictI5eX982Cyf0-z1abW8y9LAjBpTzSW4UpbcTKu4VlwqyBloo72T3qIVSsjCaM117mylC8yVcE4oBJ-D82JObv57AyJu-yHs_XDYnh4Rf_BhU4k</recordid><startdate>2005</startdate><enddate>2005</enddate><creator>Fatemi, N.S.</creator><creator>Sharma, S.</creator><creator>Buitrago, O.</creator><creator>Crisman, J.</creator><creator>Sharps, P.R.</creator><creator>Blok, R.</creator><creator>Kroon, M.</creator><creator>Jalink, Cees</creator><creator>Harris, R.</creator><creator>Stella, P.</creator><creator>Distefano, S.</creator><general>IEEE</general><scope>6IE</scope><scope>6IH</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIO</scope></search><sort><creationdate>2005</creationdate><title>Performance of high-efficiency advanced triple-junction solar panels for the LILT Mission Dawn</title><author>Fatemi, N.S. ; Sharma, S. ; Buitrago, O. ; Crisman, J. ; Sharps, P.R. ; Blok, R. ; Kroon, M. ; Jalink, Cees ; Harris, R. ; Stella, P. ; Distefano, S.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i175t-62409d4d273792652450b10676a94a8e83534c76626b98f6ceb539935e0ab09a3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2005</creationdate><topic>Aircraft manufacture</topic><topic>Belts</topic><topic>Gold</topic><topic>Manufacturing</topic><topic>Photovoltaic cells</topic><topic>Production</topic><topic>Space technology</topic><topic>Sun</topic><topic>Temperature</topic><topic>Testing</topic><toplevel>online_resources</toplevel><creatorcontrib>Fatemi, N.S.</creatorcontrib><creatorcontrib>Sharma, S.</creatorcontrib><creatorcontrib>Buitrago, O.</creatorcontrib><creatorcontrib>Crisman, J.</creatorcontrib><creatorcontrib>Sharps, P.R.</creatorcontrib><creatorcontrib>Blok, R.</creatorcontrib><creatorcontrib>Kroon, M.</creatorcontrib><creatorcontrib>Jalink, Cees</creatorcontrib><creatorcontrib>Harris, R.</creatorcontrib><creatorcontrib>Stella, P.</creatorcontrib><creatorcontrib>Distefano, S.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan (POP) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP) 1998-present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Fatemi, N.S.</au><au>Sharma, S.</au><au>Buitrago, O.</au><au>Crisman, J.</au><au>Sharps, P.R.</au><au>Blok, R.</au><au>Kroon, M.</au><au>Jalink, Cees</au><au>Harris, R.</au><au>Stella, P.</au><au>Distefano, S.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Performance of high-efficiency advanced triple-junction solar panels for the LILT Mission Dawn</atitle><btitle>Conference Record of the Thirty-first IEEE Photovoltaic Specialists Conference, 2005</btitle><stitle>PVSC</stitle><date>2005</date><risdate>2005</risdate><spage>618</spage><epage>621</epage><pages>618-621</pages><issn>0160-8371</issn><isbn>9780780387072</isbn><isbn>0780387074</isbn><abstract>NASA's Discovery Mission Dawn is designed to operate within the solar system's Asteroid belt, where the large distance from the sun creates a low-intensity, low-temperature (LILT) condition. To meet the mission power requirements under LILT conditions, very high-efficiency multijunction solar cells were selected to power the spacecraft to be built by Orbital Sciences Corporation (OSC) under contract to JPL. Emcore's InGaP/InGaAs/Ge advanced triple-junction (ATJ) solar cells, exhibiting an average air mass zero (AM0) efficiency of greater than 27.6% (one-sun, 28/spl deg/C), were used to populate the solar panels. The two solar array wings, to be built by Dutch Space, with 5 large-area panels each (total area of 36.4 m/sup 2/) are projected to produce between 10.3 kWe and 1.3 kWe of end-of-life (EOL) power in the 1.0 to 3.0 AU range, respectively. The details of the solar panel design, testing and power analysis are presented.</abstract><pub>IEEE</pub><doi>10.1109/PVSC.2005.1488207</doi><tpages>4</tpages></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | ISSN: 0160-8371 |
| ispartof | Conference Record of the Thirty-first IEEE Photovoltaic Specialists Conference, 2005, 2005, p.618-621 |
| issn | 0160-8371 |
| language | eng |
| recordid | cdi_ieee_primary_1488207 |
| source | IEEE Electronic Library (IEL) Conference Proceedings |
| subjects | Aircraft manufacture Belts Gold Manufacturing Photovoltaic cells Production Space technology Sun Temperature Testing |
| title | Performance of high-efficiency advanced triple-junction solar panels for the LILT Mission Dawn |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-23T18%3A21%3A53IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-ieee_6IE&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Performance%20of%20high-efficiency%20advanced%20triple-junction%20solar%20panels%20for%20the%20LILT%20Mission%20Dawn&rft.btitle=Conference%20Record%20of%20the%20Thirty-first%20IEEE%20Photovoltaic%20Specialists%20Conference,%202005&rft.au=Fatemi,%20N.S.&rft.date=2005&rft.spage=618&rft.epage=621&rft.pages=618-621&rft.issn=0160-8371&rft.isbn=9780780387072&rft.isbn_list=0780387074&rft_id=info:doi/10.1109/PVSC.2005.1488207&rft_dat=%3Cieee_6IE%3E1488207%3C/ieee_6IE%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_ieee_id=1488207&rfr_iscdi=true |