Development of structure with secondary defense function against space debris impact
In the Japanese experiment module (Kibo) of the International Space Station (ISS) under construction, the effective defense means are not established yet against an impact of space debris between 1 cm and 10 cm in diameter which cannot be observed from ground and shielded by the bumper. Then we have...
Gespeichert in:
Veröffentlicht in: | International journal of impact engineering 2003-12, Vol.29 (1), p.1-12 |
---|---|
Hauptverfasser: | , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 12 |
---|---|
container_issue | 1 |
container_start_page | 1 |
container_title | International journal of impact engineering |
container_volume | 29 |
creator | Akahoshi, Y. Kitamoto, C. Fukushige, S. Hata, H. |
description | In the Japanese experiment module (Kibo) of the International Space Station (ISS) under construction, the effective defense means are not established yet against an impact of space debris between 1 cm and 10 cm in diameter which cannot be observed from ground and shielded by the bumper. Then we have proposed a concept of a self-shielding bumper as an alternative bumper. In the previous self-shielding bumper, the self-shielding materials were put in a pressurized region, and they were subject to severe heat damage due to a hypervelocity impact. In this paper, we put them in vacuum between the front bumper and the rear wall (pressurized wall) in the Stuffed Whipple type bumper. And this test is evaluated using a new evaluation equation, we proposed the most effective installation position and method of the self-shielding materials. |
doi_str_mv | 10.1016/j.ijimpeng.2003.09.005 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_27849481</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0734743X03001106</els_id><sourcerecordid>27849481</sourcerecordid><originalsourceid>FETCH-LOGICAL-c372t-74d9c545a46c8a187ecc8e1d60f486684eb77f9ebe6acf8ea03bff65248d2eb93</originalsourceid><addsrcrecordid>eNqFkM1O5DAQhC20SMwOvALyiduEduLE9g3E8ichcQGJm-U4bfBoxgm2A-LtMZrlPKc-dFWp6iPklEHFgHXn68qv_XbC8FrVAE0FqgJoD8iCSaFWTQvqD1mAaPhK8ObliPxNaQ3ABLSwIE__8AM347TFkOnoaMpxtnmOSD99fqMJ7RgGE7_ogA5DQurmYLMfAzWvxoeUaZqMxfLuo0-09DA2H5NDZzYJT_7fJXm-uX66uls9PN7eX10-rGwj6lzqDMq2vDW8s9KUtmitRDZ04LjsOsmxF8Ip7LEz1kk00PTOdW3N5VBjr5olOdvlTnF8nzFlvfXJ4mZjAo5z0rWQXHHJ9gqZqlvRFkZL0u2ENo4pRXR6in5b9msG-oe2Xutf2vqHtgalC-1ivNgZsez98Bh1sh6DxcFHtFkPo98X8Q0yho5x</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>19257507</pqid></control><display><type>article</type><title>Development of structure with secondary defense function against space debris impact</title><source>Elsevier ScienceDirect Journals</source><creator>Akahoshi, Y. ; Kitamoto, C. ; Fukushige, S. ; Hata, H.</creator><creatorcontrib>Akahoshi, Y. ; Kitamoto, C. ; Fukushige, S. ; Hata, H.</creatorcontrib><description>In the Japanese experiment module (Kibo) of the International Space Station (ISS) under construction, the effective defense means are not established yet against an impact of space debris between 1 cm and 10 cm in diameter which cannot be observed from ground and shielded by the bumper. Then we have proposed a concept of a self-shielding bumper as an alternative bumper. In the previous self-shielding bumper, the self-shielding materials were put in a pressurized region, and they were subject to severe heat damage due to a hypervelocity impact. In this paper, we put them in vacuum between the front bumper and the rear wall (pressurized wall) in the Stuffed Whipple type bumper. And this test is evaluated using a new evaluation equation, we proposed the most effective installation position and method of the self-shielding materials.</description><identifier>ISSN: 0734-743X</identifier><identifier>EISSN: 1879-3509</identifier><identifier>DOI: 10.1016/j.ijimpeng.2003.09.005</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>impact analysis ; space debris</subject><ispartof>International journal of impact engineering, 2003-12, Vol.29 (1), p.1-12</ispartof><rights>2004 Elsevier Ltd</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c372t-74d9c545a46c8a187ecc8e1d60f486684eb77f9ebe6acf8ea03bff65248d2eb93</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0734743X03001106$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65534</link.rule.ids></links><search><creatorcontrib>Akahoshi, Y.</creatorcontrib><creatorcontrib>Kitamoto, C.</creatorcontrib><creatorcontrib>Fukushige, S.</creatorcontrib><creatorcontrib>Hata, H.</creatorcontrib><title>Development of structure with secondary defense function against space debris impact</title><title>International journal of impact engineering</title><description>In the Japanese experiment module (Kibo) of the International Space Station (ISS) under construction, the effective defense means are not established yet against an impact of space debris between 1 cm and 10 cm in diameter which cannot be observed from ground and shielded by the bumper. Then we have proposed a concept of a self-shielding bumper as an alternative bumper. In the previous self-shielding bumper, the self-shielding materials were put in a pressurized region, and they were subject to severe heat damage due to a hypervelocity impact. In this paper, we put them in vacuum between the front bumper and the rear wall (pressurized wall) in the Stuffed Whipple type bumper. And this test is evaluated using a new evaluation equation, we proposed the most effective installation position and method of the self-shielding materials.</description><subject>impact analysis</subject><subject>space debris</subject><issn>0734-743X</issn><issn>1879-3509</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2003</creationdate><recordtype>article</recordtype><recordid>eNqFkM1O5DAQhC20SMwOvALyiduEduLE9g3E8ichcQGJm-U4bfBoxgm2A-LtMZrlPKc-dFWp6iPklEHFgHXn68qv_XbC8FrVAE0FqgJoD8iCSaFWTQvqD1mAaPhK8ObliPxNaQ3ABLSwIE__8AM347TFkOnoaMpxtnmOSD99fqMJ7RgGE7_ogA5DQurmYLMfAzWvxoeUaZqMxfLuo0-09DA2H5NDZzYJT_7fJXm-uX66uls9PN7eX10-rGwj6lzqDMq2vDW8s9KUtmitRDZ04LjsOsmxF8Ip7LEz1kk00PTOdW3N5VBjr5olOdvlTnF8nzFlvfXJ4mZjAo5z0rWQXHHJ9gqZqlvRFkZL0u2ENo4pRXR6in5b9msG-oe2Xutf2vqHtgalC-1ivNgZsez98Bh1sh6DxcFHtFkPo98X8Q0yho5x</recordid><startdate>20031201</startdate><enddate>20031201</enddate><creator>Akahoshi, Y.</creator><creator>Kitamoto, C.</creator><creator>Fukushige, S.</creator><creator>Hata, H.</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7T2</scope><scope>7U2</scope><scope>C1K</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope></search><sort><creationdate>20031201</creationdate><title>Development of structure with secondary defense function against space debris impact</title><author>Akahoshi, Y. ; Kitamoto, C. ; Fukushige, S. ; Hata, H.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c372t-74d9c545a46c8a187ecc8e1d60f486684eb77f9ebe6acf8ea03bff65248d2eb93</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2003</creationdate><topic>impact analysis</topic><topic>space debris</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Akahoshi, Y.</creatorcontrib><creatorcontrib>Kitamoto, C.</creatorcontrib><creatorcontrib>Fukushige, S.</creatorcontrib><creatorcontrib>Hata, H.</creatorcontrib><collection>CrossRef</collection><collection>Health and Safety Science Abstracts (Full archive)</collection><collection>Safety Science and Risk</collection><collection>Environmental Sciences and Pollution Management</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><jtitle>International journal of impact engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Akahoshi, Y.</au><au>Kitamoto, C.</au><au>Fukushige, S.</au><au>Hata, H.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Development of structure with secondary defense function against space debris impact</atitle><jtitle>International journal of impact engineering</jtitle><date>2003-12-01</date><risdate>2003</risdate><volume>29</volume><issue>1</issue><spage>1</spage><epage>12</epage><pages>1-12</pages><issn>0734-743X</issn><eissn>1879-3509</eissn><abstract>In the Japanese experiment module (Kibo) of the International Space Station (ISS) under construction, the effective defense means are not established yet against an impact of space debris between 1 cm and 10 cm in diameter which cannot be observed from ground and shielded by the bumper. Then we have proposed a concept of a self-shielding bumper as an alternative bumper. In the previous self-shielding bumper, the self-shielding materials were put in a pressurized region, and they were subject to severe heat damage due to a hypervelocity impact. In this paper, we put them in vacuum between the front bumper and the rear wall (pressurized wall) in the Stuffed Whipple type bumper. And this test is evaluated using a new evaluation equation, we proposed the most effective installation position and method of the self-shielding materials.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.ijimpeng.2003.09.005</doi><tpages>12</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0734-743X |
ispartof | International journal of impact engineering, 2003-12, Vol.29 (1), p.1-12 |
issn | 0734-743X 1879-3509 |
language | eng |
recordid | cdi_proquest_miscellaneous_27849481 |
source | Elsevier ScienceDirect Journals |
subjects | impact analysis space debris |
title | Development of structure with secondary defense function against space debris impact |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-15T06%3A33%3A57IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Development%20of%20structure%20with%20secondary%20defense%20function%20against%20space%20debris%20impact&rft.jtitle=International%20journal%20of%20impact%20engineering&rft.au=Akahoshi,%20Y.&rft.date=2003-12-01&rft.volume=29&rft.issue=1&rft.spage=1&rft.epage=12&rft.pages=1-12&rft.issn=0734-743X&rft.eissn=1879-3509&rft_id=info:doi/10.1016/j.ijimpeng.2003.09.005&rft_dat=%3Cproquest_cross%3E27849481%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=19257507&rft_id=info:pmid/&rft_els_id=S0734743X03001106&rfr_iscdi=true |