One-time flight-based comprehensive analysis method for various thermal protection materials
The invention discloses a one-time flight-based comprehensive analysis method for various thermal protection materials. The comprehensive analysis method is characterized by comprising the following steps: 1, installing an ultrahigh-temperature ceramic material in a first groove, installing a first...
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creator | CUI ZHANZHONG ZHANG JIANMIN MA BAOHAI YANG HONGLIANG CHU LIMIN LI XIAO ZHOU YONGPING TAN MEIJING LIU GUOQIAN SUN XUEGONG CHEN WEIHUA CHEN JUN XU CONG |
description | The invention discloses a one-time flight-based comprehensive analysis method for various thermal protection materials. The comprehensive analysis method is characterized by comprising the following steps: 1, installing an ultrahigh-temperature ceramic material in a first groove, installing a first C/SiC material in a second groove, installing an anti-oxidization carbon/carbon material in a third groove, and installing a second C/SiC material in a fourth groove; 2, arranging three temperature sensors spaced from geometric nose lines at different depths; 3, calculating to obtain a heat flow variation according to a pneumatic heat value, and comparing the heat flow variation with the heat flow variations of the geometric nose lines of the ultrahigh-temperature ceramic material, the first C/SiC material, the anti-oxidization carbon/carbon material and the second C/SiC material, thus obtaining the catalysis characteristics of the ultrahigh-temperature ceramic material, the first C/SiC material, the anti-oxidizati |
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The comprehensive analysis method is characterized by comprising the following steps: 1, installing an ultrahigh-temperature ceramic material in a first groove, installing a first C/SiC material in a second groove, installing an anti-oxidization carbon/carbon material in a third groove, and installing a second C/SiC material in a fourth groove; 2, arranging three temperature sensors spaced from geometric nose lines at different depths; 3, calculating to obtain a heat flow variation according to a pneumatic heat value, and comparing the heat flow variation with the heat flow variations of the geometric nose lines of the ultrahigh-temperature ceramic material, the first C/SiC material, the anti-oxidization carbon/carbon material and the second C/SiC material, thus obtaining the catalysis characteristics of the ultrahigh-temperature ceramic material, the first C/SiC material, the anti-oxidizati</description><language>chi ; eng</language><subject>INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES ; MEASURING ; PHYSICS ; TESTING</subject><creationdate>2017</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170613&DB=EPODOC&CC=CN&NR=106841288A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170613&DB=EPODOC&CC=CN&NR=106841288A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CUI ZHANZHONG</creatorcontrib><creatorcontrib>ZHANG JIANMIN</creatorcontrib><creatorcontrib>MA BAOHAI</creatorcontrib><creatorcontrib>YANG HONGLIANG</creatorcontrib><creatorcontrib>CHU LIMIN</creatorcontrib><creatorcontrib>LI XIAO</creatorcontrib><creatorcontrib>ZHOU YONGPING</creatorcontrib><creatorcontrib>TAN MEIJING</creatorcontrib><creatorcontrib>LIU GUOQIAN</creatorcontrib><creatorcontrib>SUN XUEGONG</creatorcontrib><creatorcontrib>CHEN WEIHUA</creatorcontrib><creatorcontrib>CHEN JUN</creatorcontrib><creatorcontrib>XU CONG</creatorcontrib><title>One-time flight-based comprehensive analysis method for various thermal protection materials</title><description>The invention discloses a one-time flight-based comprehensive analysis method for various thermal protection materials. 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The comprehensive analysis method is characterized by comprising the following steps: 1, installing an ultrahigh-temperature ceramic material in a first groove, installing a first C/SiC material in a second groove, installing an anti-oxidization carbon/carbon material in a third groove, and installing a second C/SiC material in a fourth groove; 2, arranging three temperature sensors spaced from geometric nose lines at different depths; 3, calculating to obtain a heat flow variation according to a pneumatic heat value, and comparing the heat flow variation with the heat flow variations of the geometric nose lines of the ultrahigh-temperature ceramic material, the first C/SiC material, the anti-oxidization carbon/carbon material and the second C/SiC material, thus obtaining the catalysis characteristics of the ultrahigh-temperature ceramic material, the first C/SiC material, the anti-oxidizati</abstract><oa>free_for_read</oa></addata></record> |
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subjects | INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES MEASURING PHYSICS TESTING |
title | One-time flight-based comprehensive analysis method for various thermal protection materials |
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