New GEO paradigm: Re-purposing satellite components from the GEO graveyard
The rising production rate of space debris poses an increasingly severe threat of collision to satellites in the crowded Geostationary Orbit (GEO). It also presents a unique opportunity to make use of a growing supply of in-space resources for the benefit of the satellite community. “The Recycler” i...
Gespeichert in:
Veröffentlicht in: | Acta astronautica 2020-08, Vol.173, p.155-163 |
---|---|
Hauptverfasser: | , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 163 |
---|---|
container_issue | |
container_start_page | 155 |
container_title | Acta astronautica |
container_volume | 173 |
creator | Barbara, Nicholas H. Lizy-Destrez, Stéphanie Guardabasso, Paolo Alary, Didier |
description | The rising production rate of space debris poses an increasingly severe threat of collision to satellites in the crowded Geostationary Orbit (GEO). It also presents a unique opportunity to make use of a growing supply of in-space resources for the benefit of the satellite community. “The Recycler” is a mission proposed to source replacements for failed components in GEO satellites by extracting functioning components from non-operational spacecraft in the GEO graveyard. This paper demonstrates a method of analyzing in-space re-purposing missions such as the Recycler, using real satellite data to provide a strong platform for accurate performance estimates. An inventory of 1107 satellites in the extended GEO region is presented, and a review into past GEO satellite anomalies is conducted to show that solar arrays would be in the greatest demand for re-purposing. This inventory is used as an input to a greedy selection algorithm and trajectory simulation to show that the Recycler spacecraft could harvest components for 67 client satellites with its allotted fuel budget. This capacity directly meets the levels of customer demand estimated from the GEO satellite anomaly data, placing the Recycler as a strong contender in a future second-hand satellite-component industry. Propellant mass is found to be a greater restriction on the Recycler mission than its 15-year lifetime — a problem which could be solved by on-orbit refueling.
•Satellite databases are critical when designing on-orbit servicing missions.•On-orbit re-purposing missions should focus on solar arrays in Geostationary Orbit.•Multi-target trajectory optimization is used to predict the Recycler's performance.•The Recycler can visit 67 satellites using electric propulsion with its fuel budget.•On-orbit refueling is essential for sustainable satellite-servicing missions. |
doi_str_mv | 10.1016/j.actaastro.2020.03.041 |
format | Article |
fullrecord | <record><control><sourceid>proquest_hal_p</sourceid><recordid>TN_cdi_hal_primary_oai_HAL_hal_03200249v1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0094576520301697</els_id><sourcerecordid>2440679535</sourcerecordid><originalsourceid>FETCH-LOGICAL-c426t-7e72204c8e0821ae70266e8fc45a1634c2d3c19233a6cc03b495a45a6d1716d53</originalsourceid><addsrcrecordid>eNqFkE1LAzEQhoMoWD9-gwuePOw6-dhk11uR2irFgug5xOy0prSbNUkr_nu3Vnr1NDDzvs_MvIRcUSgoUHm7LIxNxsQUfMGAQQG8AEGPyIBWqs4ZcDgmA4Ba5KWS5Sk5i3EJAIpV9YA8PeNXNh7Nss4E07jF-i57wbzbhM5H1y6yaBKuVi5hZv268y22KWbz4NdZ-sBf4yKYLX6b0FyQk7lZRbz8q-fk7WH0ej_Jp7Px4_1wmlvBZMoVKsZA2AqhYtSgAiYlVnMrSkMlF5Y13NKacW6ktcDfRV2afiYbqqhsSn5ObvbcD7PSXXBrE761N05PhlO96wFnAEzUW9prr_faLvjPDcakl34T2v48zYQAqeqS74hqr7LBxxhwfsBS0LuQ9VIfQta7kPsdug-5dw73Tuwf3joMOlqHrcXGBbRJN979y_gB_TGHOA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2440679535</pqid></control><display><type>article</type><title>New GEO paradigm: Re-purposing satellite components from the GEO graveyard</title><source>Elsevier ScienceDirect Journals Complete</source><creator>Barbara, Nicholas H. ; Lizy-Destrez, Stéphanie ; Guardabasso, Paolo ; Alary, Didier</creator><creatorcontrib>Barbara, Nicholas H. ; Lizy-Destrez, Stéphanie ; Guardabasso, Paolo ; Alary, Didier</creatorcontrib><description>The rising production rate of space debris poses an increasingly severe threat of collision to satellites in the crowded Geostationary Orbit (GEO). It also presents a unique opportunity to make use of a growing supply of in-space resources for the benefit of the satellite community. “The Recycler” is a mission proposed to source replacements for failed components in GEO satellites by extracting functioning components from non-operational spacecraft in the GEO graveyard. This paper demonstrates a method of analyzing in-space re-purposing missions such as the Recycler, using real satellite data to provide a strong platform for accurate performance estimates. An inventory of 1107 satellites in the extended GEO region is presented, and a review into past GEO satellite anomalies is conducted to show that solar arrays would be in the greatest demand for re-purposing. This inventory is used as an input to a greedy selection algorithm and trajectory simulation to show that the Recycler spacecraft could harvest components for 67 client satellites with its allotted fuel budget. This capacity directly meets the levels of customer demand estimated from the GEO satellite anomaly data, placing the Recycler as a strong contender in a future second-hand satellite-component industry. Propellant mass is found to be a greater restriction on the Recycler mission than its 15-year lifetime — a problem which could be solved by on-orbit refueling.
•Satellite databases are critical when designing on-orbit servicing missions.•On-orbit re-purposing missions should focus on solar arrays in Geostationary Orbit.•Multi-target trajectory optimization is used to predict the Recycler's performance.•The Recycler can visit 67 satellites using electric propulsion with its fuel budget.•On-orbit refueling is essential for sustainable satellite-servicing missions.</description><identifier>ISSN: 0094-5765</identifier><identifier>EISSN: 1879-2030</identifier><identifier>DOI: 10.1016/j.actaastro.2020.03.041</identifier><language>eng</language><publisher>Elmsford: Elsevier Ltd</publisher><subject>Anomalies ; Cemeteries ; Computer simulation ; Engineering Sciences ; GEO ; Geosynchronous orbits ; Greedy algorithms ; On-orbit servicing ; Other ; Re-purposing ; Satellite data ; Satellite database ; Satellites ; Solar arrays ; Solar collectors ; Space debris ; Spacecraft</subject><ispartof>Acta astronautica, 2020-08, Vol.173, p.155-163</ispartof><rights>2020 IAA</rights><rights>Copyright Elsevier BV Aug 2020</rights><rights>Distributed under a Creative Commons Attribution 4.0 International License</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c426t-7e72204c8e0821ae70266e8fc45a1634c2d3c19233a6cc03b495a45a6d1716d53</citedby><cites>FETCH-LOGICAL-c426t-7e72204c8e0821ae70266e8fc45a1634c2d3c19233a6cc03b495a45a6d1716d53</cites><orcidid>0000-0001-8304-7178 ; 0000-0002-4885-3307 ; 0000-0001-8634-2340</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0094576520301697$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>230,314,776,780,881,3537,27901,27902,65534</link.rule.ids><backlink>$$Uhttps://hal.science/hal-03200249$$DView record in HAL$$Hfree_for_read</backlink></links><search><creatorcontrib>Barbara, Nicholas H.</creatorcontrib><creatorcontrib>Lizy-Destrez, Stéphanie</creatorcontrib><creatorcontrib>Guardabasso, Paolo</creatorcontrib><creatorcontrib>Alary, Didier</creatorcontrib><title>New GEO paradigm: Re-purposing satellite components from the GEO graveyard</title><title>Acta astronautica</title><description>The rising production rate of space debris poses an increasingly severe threat of collision to satellites in the crowded Geostationary Orbit (GEO). It also presents a unique opportunity to make use of a growing supply of in-space resources for the benefit of the satellite community. “The Recycler” is a mission proposed to source replacements for failed components in GEO satellites by extracting functioning components from non-operational spacecraft in the GEO graveyard. This paper demonstrates a method of analyzing in-space re-purposing missions such as the Recycler, using real satellite data to provide a strong platform for accurate performance estimates. An inventory of 1107 satellites in the extended GEO region is presented, and a review into past GEO satellite anomalies is conducted to show that solar arrays would be in the greatest demand for re-purposing. This inventory is used as an input to a greedy selection algorithm and trajectory simulation to show that the Recycler spacecraft could harvest components for 67 client satellites with its allotted fuel budget. This capacity directly meets the levels of customer demand estimated from the GEO satellite anomaly data, placing the Recycler as a strong contender in a future second-hand satellite-component industry. Propellant mass is found to be a greater restriction on the Recycler mission than its 15-year lifetime — a problem which could be solved by on-orbit refueling.
•Satellite databases are critical when designing on-orbit servicing missions.•On-orbit re-purposing missions should focus on solar arrays in Geostationary Orbit.•Multi-target trajectory optimization is used to predict the Recycler's performance.•The Recycler can visit 67 satellites using electric propulsion with its fuel budget.•On-orbit refueling is essential for sustainable satellite-servicing missions.</description><subject>Anomalies</subject><subject>Cemeteries</subject><subject>Computer simulation</subject><subject>Engineering Sciences</subject><subject>GEO</subject><subject>Geosynchronous orbits</subject><subject>Greedy algorithms</subject><subject>On-orbit servicing</subject><subject>Other</subject><subject>Re-purposing</subject><subject>Satellite data</subject><subject>Satellite database</subject><subject>Satellites</subject><subject>Solar arrays</subject><subject>Solar collectors</subject><subject>Space debris</subject><subject>Spacecraft</subject><issn>0094-5765</issn><issn>1879-2030</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNqFkE1LAzEQhoMoWD9-gwuePOw6-dhk11uR2irFgug5xOy0prSbNUkr_nu3Vnr1NDDzvs_MvIRcUSgoUHm7LIxNxsQUfMGAQQG8AEGPyIBWqs4ZcDgmA4Ba5KWS5Sk5i3EJAIpV9YA8PeNXNh7Nss4E07jF-i57wbzbhM5H1y6yaBKuVi5hZv268y22KWbz4NdZ-sBf4yKYLX6b0FyQk7lZRbz8q-fk7WH0ej_Jp7Px4_1wmlvBZMoVKsZA2AqhYtSgAiYlVnMrSkMlF5Y13NKacW6ktcDfRV2afiYbqqhsSn5ObvbcD7PSXXBrE761N05PhlO96wFnAEzUW9prr_faLvjPDcakl34T2v48zYQAqeqS74hqr7LBxxhwfsBS0LuQ9VIfQta7kPsdug-5dw73Tuwf3joMOlqHrcXGBbRJN979y_gB_TGHOA</recordid><startdate>202008</startdate><enddate>202008</enddate><creator>Barbara, Nicholas H.</creator><creator>Lizy-Destrez, Stéphanie</creator><creator>Guardabasso, Paolo</creator><creator>Alary, Didier</creator><general>Elsevier Ltd</general><general>Elsevier BV</general><general>Elsevier</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>7TG</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>KL.</scope><scope>L7M</scope><scope>1XC</scope><scope>VOOES</scope><orcidid>https://orcid.org/0000-0001-8304-7178</orcidid><orcidid>https://orcid.org/0000-0002-4885-3307</orcidid><orcidid>https://orcid.org/0000-0001-8634-2340</orcidid></search><sort><creationdate>202008</creationdate><title>New GEO paradigm: Re-purposing satellite components from the GEO graveyard</title><author>Barbara, Nicholas H. ; Lizy-Destrez, Stéphanie ; Guardabasso, Paolo ; Alary, Didier</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c426t-7e72204c8e0821ae70266e8fc45a1634c2d3c19233a6cc03b495a45a6d1716d53</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Anomalies</topic><topic>Cemeteries</topic><topic>Computer simulation</topic><topic>Engineering Sciences</topic><topic>GEO</topic><topic>Geosynchronous orbits</topic><topic>Greedy algorithms</topic><topic>On-orbit servicing</topic><topic>Other</topic><topic>Re-purposing</topic><topic>Satellite data</topic><topic>Satellite database</topic><topic>Satellites</topic><topic>Solar arrays</topic><topic>Solar collectors</topic><topic>Space debris</topic><topic>Spacecraft</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Barbara, Nicholas H.</creatorcontrib><creatorcontrib>Lizy-Destrez, Stéphanie</creatorcontrib><creatorcontrib>Guardabasso, Paolo</creatorcontrib><creatorcontrib>Alary, Didier</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Meteorological & Geoastrophysical Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Meteorological & Geoastrophysical Abstracts - Academic</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Hyper Article en Ligne (HAL)</collection><collection>Hyper Article en Ligne (HAL) (Open Access)</collection><jtitle>Acta astronautica</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Barbara, Nicholas H.</au><au>Lizy-Destrez, Stéphanie</au><au>Guardabasso, Paolo</au><au>Alary, Didier</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>New GEO paradigm: Re-purposing satellite components from the GEO graveyard</atitle><jtitle>Acta astronautica</jtitle><date>2020-08</date><risdate>2020</risdate><volume>173</volume><spage>155</spage><epage>163</epage><pages>155-163</pages><issn>0094-5765</issn><eissn>1879-2030</eissn><abstract>The rising production rate of space debris poses an increasingly severe threat of collision to satellites in the crowded Geostationary Orbit (GEO). It also presents a unique opportunity to make use of a growing supply of in-space resources for the benefit of the satellite community. “The Recycler” is a mission proposed to source replacements for failed components in GEO satellites by extracting functioning components from non-operational spacecraft in the GEO graveyard. This paper demonstrates a method of analyzing in-space re-purposing missions such as the Recycler, using real satellite data to provide a strong platform for accurate performance estimates. An inventory of 1107 satellites in the extended GEO region is presented, and a review into past GEO satellite anomalies is conducted to show that solar arrays would be in the greatest demand for re-purposing. This inventory is used as an input to a greedy selection algorithm and trajectory simulation to show that the Recycler spacecraft could harvest components for 67 client satellites with its allotted fuel budget. This capacity directly meets the levels of customer demand estimated from the GEO satellite anomaly data, placing the Recycler as a strong contender in a future second-hand satellite-component industry. Propellant mass is found to be a greater restriction on the Recycler mission than its 15-year lifetime — a problem which could be solved by on-orbit refueling.
•Satellite databases are critical when designing on-orbit servicing missions.•On-orbit re-purposing missions should focus on solar arrays in Geostationary Orbit.•Multi-target trajectory optimization is used to predict the Recycler's performance.•The Recycler can visit 67 satellites using electric propulsion with its fuel budget.•On-orbit refueling is essential for sustainable satellite-servicing missions.</abstract><cop>Elmsford</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.actaastro.2020.03.041</doi><tpages>9</tpages><orcidid>https://orcid.org/0000-0001-8304-7178</orcidid><orcidid>https://orcid.org/0000-0002-4885-3307</orcidid><orcidid>https://orcid.org/0000-0001-8634-2340</orcidid><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0094-5765 |
ispartof | Acta astronautica, 2020-08, Vol.173, p.155-163 |
issn | 0094-5765 1879-2030 |
language | eng |
recordid | cdi_hal_primary_oai_HAL_hal_03200249v1 |
source | Elsevier ScienceDirect Journals Complete |
subjects | Anomalies Cemeteries Computer simulation Engineering Sciences GEO Geosynchronous orbits Greedy algorithms On-orbit servicing Other Re-purposing Satellite data Satellite database Satellites Solar arrays Solar collectors Space debris Spacecraft |
title | New GEO paradigm: Re-purposing satellite components from the GEO graveyard |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-14T09%3A34%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_hal_p&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=New%20GEO%20paradigm:%20Re-purposing%20satellite%20components%20from%20the%20GEO%20graveyard&rft.jtitle=Acta%20astronautica&rft.au=Barbara,%20Nicholas%20H.&rft.date=2020-08&rft.volume=173&rft.spage=155&rft.epage=163&rft.pages=155-163&rft.issn=0094-5765&rft.eissn=1879-2030&rft_id=info:doi/10.1016/j.actaastro.2020.03.041&rft_dat=%3Cproquest_hal_p%3E2440679535%3C/proquest_hal_p%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2440679535&rft_id=info:pmid/&rft_els_id=S0094576520301697&rfr_iscdi=true |