Loading…
Long-Term Exposure of Adhesively Bonded Thin Polymer Composite Laminates in Low Earth Orbit Environment
A summary of the results of the long-term passive exposure of adhesively bonded joints of polymer composite laminates on the outboard of the Mir space station and the in situ experiment on the functional cargo block of the International Space Station are presented. Crack resistance, structure and pr...
Saved in:
Published in: | High performance polymers 2001-09, Vol.13 (3), p.S461-S466 |
---|---|
Main Authors: | , , , |
Format: | Article |
Language: | English |
Citations: | Items that this one cites |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | |
---|---|
cites | cdi_FETCH-LOGICAL-c258t-1882decd9173ec59ef174a9691b4c1498e9096e42764b3d3d53afeec3db9c1af3 |
container_end_page | S466 |
container_issue | 3 |
container_start_page | S461 |
container_title | High performance polymers |
container_volume | 13 |
creator | Babayevsky, Petr G Kozlov, Nicolai A Shubin, Alexander N Smirnova, Tatiyana N |
description | A summary of the results of the long-term passive exposure of adhesively bonded joints of polymer composite laminates on the outboard of the Mir space station and the in situ experiment on the functional cargo block of the International Space Station are presented. Crack resistance, structure and properties of the adhesive joints were examined after passive exposure. Subcritical crack propagation control in the same type of adhesively bonded joints was carried out during the experiment in outer space. It was shown that the long-term exposure increases the brittleness of the adhesive joints due to postcuring processes, elimination of low molecular weight components and interphase damage formation. The subcritical crack propagation velocity is of the same order as on-ground check tests, but can occur under lower G
I
values. |
doi_str_mv | 10.1088/0954-0083/13/3/337 |
format | article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_34983622</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>26781307</sourcerecordid><originalsourceid>FETCH-LOGICAL-c258t-1882decd9173ec59ef174a9691b4c1498e9096e42764b3d3d53afeec3db9c1af3</originalsourceid><addsrcrecordid>eNqFkL1OwzAYRS0EEqXwAkye2EL9xfmxx1KFHylSGcpsuc6X1iixi50W-vakArGiO9zhHt3hEHIL7B6YEDMm8yxhTPAZ8NkYXp6RCfACkiKD9JxM_oBLchXjO2MAAvIJ2dTebZIVhp5WXzsf9wGpb-m82WK0B-yO9MG7Bhu62lpHX3137DHQhe9H1g5Ia91bpweMdJxr_0krHYYtXYa1HWjlDjZ416MbrslFq7uIN789JW-P1WrxnNTLp5fFvE5MmoshASHSBk0joeRocoktlJmWhYR1ZiCTAiWTBWZpWWRr3vAm57pFNLxZSwO65VNy9_O7C_5jj3FQvY0Gu0479Puo-PjBizT9F0yLUgBn5QimP6AJPsaArdoF2-twVMDUSb46uVUntwq4GsNL_g2k_Xgs</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>26781307</pqid></control><display><type>article</type><title>Long-Term Exposure of Adhesively Bonded Thin Polymer Composite Laminates in Low Earth Orbit Environment</title><source>Sage Journals Online</source><creator>Babayevsky, Petr G ; Kozlov, Nicolai A ; Shubin, Alexander N ; Smirnova, Tatiyana N</creator><creatorcontrib>Babayevsky, Petr G ; Kozlov, Nicolai A ; Shubin, Alexander N ; Smirnova, Tatiyana N</creatorcontrib><description>A summary of the results of the long-term passive exposure of adhesively bonded joints of polymer composite laminates on the outboard of the Mir space station and the in situ experiment on the functional cargo block of the International Space Station are presented. Crack resistance, structure and properties of the adhesive joints were examined after passive exposure. Subcritical crack propagation control in the same type of adhesively bonded joints was carried out during the experiment in outer space. It was shown that the long-term exposure increases the brittleness of the adhesive joints due to postcuring processes, elimination of low molecular weight components and interphase damage formation. The subcritical crack propagation velocity is of the same order as on-ground check tests, but can occur under lower G
I
values.</description><identifier>ISSN: 0954-0083</identifier><identifier>EISSN: 1361-6412</identifier><identifier>DOI: 10.1088/0954-0083/13/3/337</identifier><language>eng</language><ispartof>High performance polymers, 2001-09, Vol.13 (3), p.S461-S466</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c258t-1882decd9173ec59ef174a9691b4c1498e9096e42764b3d3d53afeec3db9c1af3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904</link.rule.ids></links><search><creatorcontrib>Babayevsky, Petr G</creatorcontrib><creatorcontrib>Kozlov, Nicolai A</creatorcontrib><creatorcontrib>Shubin, Alexander N</creatorcontrib><creatorcontrib>Smirnova, Tatiyana N</creatorcontrib><title>Long-Term Exposure of Adhesively Bonded Thin Polymer Composite Laminates in Low Earth Orbit Environment</title><title>High performance polymers</title><description>A summary of the results of the long-term passive exposure of adhesively bonded joints of polymer composite laminates on the outboard of the Mir space station and the in situ experiment on the functional cargo block of the International Space Station are presented. Crack resistance, structure and properties of the adhesive joints were examined after passive exposure. Subcritical crack propagation control in the same type of adhesively bonded joints was carried out during the experiment in outer space. It was shown that the long-term exposure increases the brittleness of the adhesive joints due to postcuring processes, elimination of low molecular weight components and interphase damage formation. The subcritical crack propagation velocity is of the same order as on-ground check tests, but can occur under lower G
I
values.</description><issn>0954-0083</issn><issn>1361-6412</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2001</creationdate><recordtype>article</recordtype><recordid>eNqFkL1OwzAYRS0EEqXwAkye2EL9xfmxx1KFHylSGcpsuc6X1iixi50W-vakArGiO9zhHt3hEHIL7B6YEDMm8yxhTPAZ8NkYXp6RCfACkiKD9JxM_oBLchXjO2MAAvIJ2dTebZIVhp5WXzsf9wGpb-m82WK0B-yO9MG7Bhu62lpHX3137DHQhe9H1g5Ia91bpweMdJxr_0krHYYtXYa1HWjlDjZ416MbrslFq7uIN789JW-P1WrxnNTLp5fFvE5MmoshASHSBk0joeRocoktlJmWhYR1ZiCTAiWTBWZpWWRr3vAm57pFNLxZSwO65VNy9_O7C_5jj3FQvY0Gu0479Puo-PjBizT9F0yLUgBn5QimP6AJPsaArdoF2-twVMDUSb46uVUntwq4GsNL_g2k_Xgs</recordid><startdate>20010901</startdate><enddate>20010901</enddate><creator>Babayevsky, Petr G</creator><creator>Kozlov, Nicolai A</creator><creator>Shubin, Alexander N</creator><creator>Smirnova, Tatiyana N</creator><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>7SR</scope><scope>JG9</scope></search><sort><creationdate>20010901</creationdate><title>Long-Term Exposure of Adhesively Bonded Thin Polymer Composite Laminates in Low Earth Orbit Environment</title><author>Babayevsky, Petr G ; Kozlov, Nicolai A ; Shubin, Alexander N ; Smirnova, Tatiyana N</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c258t-1882decd9173ec59ef174a9691b4c1498e9096e42764b3d3d53afeec3db9c1af3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2001</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Babayevsky, Petr G</creatorcontrib><creatorcontrib>Kozlov, Nicolai A</creatorcontrib><creatorcontrib>Shubin, Alexander N</creatorcontrib><creatorcontrib>Smirnova, Tatiyana N</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Engineered Materials Abstracts</collection><collection>Materials Research Database</collection><jtitle>High performance polymers</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Babayevsky, Petr G</au><au>Kozlov, Nicolai A</au><au>Shubin, Alexander N</au><au>Smirnova, Tatiyana N</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Long-Term Exposure of Adhesively Bonded Thin Polymer Composite Laminates in Low Earth Orbit Environment</atitle><jtitle>High performance polymers</jtitle><date>2001-09-01</date><risdate>2001</risdate><volume>13</volume><issue>3</issue><spage>S461</spage><epage>S466</epage><pages>S461-S466</pages><issn>0954-0083</issn><eissn>1361-6412</eissn><abstract>A summary of the results of the long-term passive exposure of adhesively bonded joints of polymer composite laminates on the outboard of the Mir space station and the in situ experiment on the functional cargo block of the International Space Station are presented. Crack resistance, structure and properties of the adhesive joints were examined after passive exposure. Subcritical crack propagation control in the same type of adhesively bonded joints was carried out during the experiment in outer space. It was shown that the long-term exposure increases the brittleness of the adhesive joints due to postcuring processes, elimination of low molecular weight components and interphase damage formation. The subcritical crack propagation velocity is of the same order as on-ground check tests, but can occur under lower G
I
values.</abstract><doi>10.1088/0954-0083/13/3/337</doi></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0954-0083 |
ispartof | High performance polymers, 2001-09, Vol.13 (3), p.S461-S466 |
issn | 0954-0083 1361-6412 |
language | eng |
recordid | cdi_proquest_miscellaneous_34983622 |
source | Sage Journals Online |
title | Long-Term Exposure of Adhesively Bonded Thin Polymer Composite Laminates in Low Earth Orbit Environment |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-27T01%3A36%3A52IST&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=Long-Term%20Exposure%20of%20Adhesively%20Bonded%20Thin%20Polymer%20Composite%20Laminates%20in%20Low%20Earth%20Orbit%20Environment&rft.jtitle=High%20performance%20polymers&rft.au=Babayevsky,%20Petr%20G&rft.date=2001-09-01&rft.volume=13&rft.issue=3&rft.spage=S461&rft.epage=S466&rft.pages=S461-S466&rft.issn=0954-0083&rft.eissn=1361-6412&rft_id=info:doi/10.1088/0954-0083/13/3/337&rft_dat=%3Cproquest_cross%3E26781307%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c258t-1882decd9173ec59ef174a9691b4c1498e9096e42764b3d3d53afeec3db9c1af3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=26781307&rft_id=info:pmid/&rfr_iscdi=true |