Orbital Debris Environment Model in the Geosynchronous Region
The Kyushu University orbital debris environment model in the geosynchronous region has been updated to provide a better and more accurate description and understanding of orbital debris environment than the previous model. The main advantage of the present model over the previous model is to introd...
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Veröffentlicht in: | Journal of spacecraft and rockets 2002-01, Vol.39 (1), p.92-98 |
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creator | Hanada, Toshiya Yasaka, Tetsuo |
description | The Kyushu University orbital debris environment model in the geosynchronous region has been updated to provide a better and more accurate description and understanding of orbital debris environment than the previous model. The main advantage of the present model over the previous model is to introduce more realistic breakup dispersion to estimate collision hazards to other spacecraft caused by breakup fragments. The results from the new model indicate that all aged satellites should move into a disposal orbit at the end of mission to reduce potential hazards to operational satellites. However, boosting up all aged satellites cannot preserve the current orbital environment sufficiently because debris fragments from explosions are still hazardous to operational satellites. The results also indicate that safekeeping procedures for all rocket bodies and spacecraft that remain in the geosynchronous region after completion of their mission are required as well as in low Earth orbit. |
doi_str_mv | 10.2514/2.3786 |
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The main advantage of the present model over the previous model is to introduce more realistic breakup dispersion to estimate collision hazards to other spacecraft caused by breakup fragments. The results from the new model indicate that all aged satellites should move into a disposal orbit at the end of mission to reduce potential hazards to operational satellites. However, boosting up all aged satellites cannot preserve the current orbital environment sufficiently because debris fragments from explosions are still hazardous to operational satellites. The results also indicate that safekeeping procedures for all rocket bodies and spacecraft that remain in the geosynchronous region after completion of their mission are required as well as in low Earth orbit.</description><identifier>ISSN: 0022-4650</identifier><identifier>EISSN: 1533-6794</identifier><identifier>DOI: 10.2514/2.3786</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Collision avoidance ; Environment models ; Orbits ; Satellites ; Space debris ; Spacecraft</subject><ispartof>Journal of spacecraft and rockets, 2002-01, Vol.39 (1), p.92-98</ispartof><rights>Copyright American Institute of Aeronautics and Astronautics Jan/Feb 2002</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Hanada, Toshiya</creatorcontrib><creatorcontrib>Yasaka, Tetsuo</creatorcontrib><title>Orbital Debris Environment Model in the Geosynchronous Region</title><title>Journal of spacecraft and rockets</title><description>The Kyushu University orbital debris environment model in the geosynchronous region has been updated to provide a better and more accurate description and understanding of orbital debris environment than the previous model. The main advantage of the present model over the previous model is to introduce more realistic breakup dispersion to estimate collision hazards to other spacecraft caused by breakup fragments. The results from the new model indicate that all aged satellites should move into a disposal orbit at the end of mission to reduce potential hazards to operational satellites. However, boosting up all aged satellites cannot preserve the current orbital environment sufficiently because debris fragments from explosions are still hazardous to operational satellites. The results also indicate that safekeeping procedures for all rocket bodies and spacecraft that remain in the geosynchronous region after completion of their mission are required as well as in low Earth orbit.</description><subject>Collision avoidance</subject><subject>Environment models</subject><subject>Orbits</subject><subject>Satellites</subject><subject>Space debris</subject><subject>Spacecraft</subject><issn>0022-4650</issn><issn>1533-6794</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2002</creationdate><recordtype>article</recordtype><recordid>eNp9z81KAzEUBeAgCtaqzxAQdDU1uflfuJBaq1ApiK6HZCaxU6ZJncwIvr0junLh6i7Ox-FchM4pmYGg_BpmTGl5gCZUMFZIZfghmhACUHApyDE6yXlLCJVamgm6WXeu6W2L77zrmowX8aPpUtz52OOnVPsWNxH3G4-XPuXPWG3GMA0ZP_u3JsVTdBRsm_3Z752i1_vFy_yhWK2Xj_PbVbEHzvuiVmA458Eao4SvNQkUhFGMOu9qwyyRRDNnwQIPopI0MKIp44E5GgCcZlN09dO779L74HNf7ppc-ba10Y9rSsUloZqKb3n5rwSpjdBKjfDiD9ymoYvjFyVQSRUHwiT7AkBqYjk</recordid><startdate>20020101</startdate><enddate>20020101</enddate><creator>Hanada, Toshiya</creator><creator>Yasaka, Tetsuo</creator><general>American Institute of Aeronautics and Astronautics</general><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>7TC</scope></search><sort><creationdate>20020101</creationdate><title>Orbital Debris Environment Model in the Geosynchronous Region</title><author>Hanada, Toshiya ; Yasaka, Tetsuo</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p244t-d729444fa9975ed80f1259731bebd93a06083ba2a24f5c61f308134f3b1f22b83</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2002</creationdate><topic>Collision avoidance</topic><topic>Environment models</topic><topic>Orbits</topic><topic>Satellites</topic><topic>Space debris</topic><topic>Spacecraft</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hanada, Toshiya</creatorcontrib><creatorcontrib>Yasaka, Tetsuo</creatorcontrib><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Mechanical Engineering Abstracts</collection><jtitle>Journal of spacecraft and rockets</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hanada, Toshiya</au><au>Yasaka, Tetsuo</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Orbital Debris Environment Model in the Geosynchronous Region</atitle><jtitle>Journal of spacecraft and rockets</jtitle><date>2002-01-01</date><risdate>2002</risdate><volume>39</volume><issue>1</issue><spage>92</spage><epage>98</epage><pages>92-98</pages><issn>0022-4650</issn><eissn>1533-6794</eissn><abstract>The Kyushu University orbital debris environment model in the geosynchronous region has been updated to provide a better and more accurate description and understanding of orbital debris environment than the previous model. The main advantage of the present model over the previous model is to introduce more realistic breakup dispersion to estimate collision hazards to other spacecraft caused by breakup fragments. The results from the new model indicate that all aged satellites should move into a disposal orbit at the end of mission to reduce potential hazards to operational satellites. However, boosting up all aged satellites cannot preserve the current orbital environment sufficiently because debris fragments from explosions are still hazardous to operational satellites. The results also indicate that safekeeping procedures for all rocket bodies and spacecraft that remain in the geosynchronous region after completion of their mission are required as well as in low Earth orbit.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/2.3786</doi><tpages>7</tpages></addata></record> |
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source | Alma/SFX Local Collection |
subjects | Collision avoidance Environment models Orbits Satellites Space debris Spacecraft |
title | Orbital Debris Environment Model in the Geosynchronous Region |
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