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The influence of space environmental factors on the laser-induced damage thresholds in optical components
This paper systematically investigated the impact mechanisms of proton irradiation, atomic oxygen irradiation and space debris collision, both individually and in combination, on the laser damage threshold and damage evolution characteristics of HfO2/SiO2 triple-band high-reflection films and fused...
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Published in: | High power laser science and engineering 2024-01, Vol.12, Article e47 |
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description | This paper systematically investigated the impact mechanisms of proton irradiation, atomic oxygen irradiation and space debris collision, both individually and in combination, on the laser damage threshold and damage evolution characteristics of HfO2/SiO2 triple-band high-reflection films and fused silica substrates using a simulated near-Earth space radiation experimental system. For the high-reflection film samples, the damage thresholds decreased by 15.38%, 13.12% and 46.80% after proton, atomic oxygen and simulated space debris (penetration) irradiation, respectively. The coupling irradiation of the first two factors resulted in a decrease of 26.93%, while the combined effect of all the three factors led to a reduction of 63.19%. Similarly, the fused silica substrates exhibited the same pattern of laser damage performance degradation. Notably, the study employed high-precision fixed-point in situ measurement techniques to track in detail the microstructural changes, surface roughness and optical-thermal absorption intensity before and after proton and atomic oxygen irradiation at the same location, thus providing a more accurate and comprehensive analysis of the damage mechanisms. In addition, simulations were conducted to quantitatively analyze the transmission trajectories and concentration distribution lines of protons and atomic oxygen incident at specific angles into the target material. The research findings contribute to elucidating the laser damage performance degradation mechanism of transmissive elements in near-Earth space environments and provide technical support for the development of high-damage-threshold optical components resistant to space radiation. |
doi_str_mv | 10.1017/hpl.2024.28 |
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For the high-reflection film samples, the damage thresholds decreased by 15.38%, 13.12% and 46.80% after proton, atomic oxygen and simulated space debris (penetration) irradiation, respectively. The coupling irradiation of the first two factors resulted in a decrease of 26.93%, while the combined effect of all the three factors led to a reduction of 63.19%. Similarly, the fused silica substrates exhibited the same pattern of laser damage performance degradation. Notably, the study employed high-precision fixed-point in situ measurement techniques to track in detail the microstructural changes, surface roughness and optical-thermal absorption intensity before and after proton and atomic oxygen irradiation at the same location, thus providing a more accurate and comprehensive analysis of the damage mechanisms. In addition, simulations were conducted to quantitatively analyze the transmission trajectories and concentration distribution lines of protons and atomic oxygen incident at specific angles into the target material. The research findings contribute to elucidating the laser damage performance degradation mechanism of transmissive elements in near-Earth space environments and provide technical support for the development of high-damage-threshold optical components resistant to space radiation.</description><identifier>ISSN: 2095-4719</identifier><identifier>EISSN: 2052-3289</identifier><identifier>DOI: 10.1017/hpl.2024.28</identifier><language>eng</language><publisher>Cambridge, UK: Cambridge University Press</publisher><subject>Aerospace environments ; Atomic oxygen ; Charged particles ; Cosmic rays ; coupling effects ; Damage patterns ; Energy ; Experiments ; Extraterrestrial radiation ; Fused silica ; In situ measurement ; Laser damage ; laser-induced damage thresholds ; Lasers ; Microscopy ; Optical components ; Optics ; Performance degradation ; Proton damage ; Proton irradiation ; Radar systems ; Radiation damage ; Radiation tolerance ; Satellites ; Silicon dioxide ; Space debris ; space environments ; Substrates ; Surface roughness ; Temperature ; Thermal absorption ; Thermal cycling ; Thin films ; Thresholds ; Ultraviolet radiation ; Yield point</subject><ispartof>High power laser science and engineering, 2024-01, Vol.12, Article e47</ispartof><rights>The Author(s), 2024. Published by Cambridge University Press in association with Chinese Laser Press</rights><rights>The Author(s), 2024. Published by Cambridge University Press in association with Chinese Laser Press. This work is licensed under the Creative Commons Attribution License This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (https://creativecommons.org/licenses/by/4.0), which permits unrestricted re-use, distribution and reproduction, provided the original article is properly cited. (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><orcidid>0009-0004-5619-7305 ; 0000-0003-1188-4588</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.proquest.com/docview/3106645754/fulltextPDF?pq-origsite=primo$$EPDF$$P50$$Gproquest$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://www.proquest.com/docview/3106645754?pq-origsite=primo$$EHTML$$P50$$Gproquest$$Hfree_for_read</linktohtml><link.rule.ids>314,777,781,25734,27905,27906,36993,44571,72709,74875</link.rule.ids></links><search><creatorcontrib>Ma, Bin</creatorcontrib><creatorcontrib>Guan, Shuang</creatorcontrib><creatorcontrib>Yan, Dongyue</creatorcontrib><creatorcontrib>Pan, Qiaofei</creatorcontrib><creatorcontrib>Hou, Zhiqiang</creatorcontrib><creatorcontrib>Wang, Ke</creatorcontrib><creatorcontrib>Han, Jiaqi</creatorcontrib><title>The influence of space environmental factors on the laser-induced damage thresholds in optical components</title><title>High power laser science and engineering</title><addtitle>High Pow Laser Sci Eng</addtitle><description>This paper systematically investigated the impact mechanisms of proton irradiation, atomic oxygen irradiation and space debris collision, both individually and in combination, on the laser damage threshold and damage evolution characteristics of HfO2/SiO2 triple-band high-reflection films and fused silica substrates using a simulated near-Earth space radiation experimental system. For the high-reflection film samples, the damage thresholds decreased by 15.38%, 13.12% and 46.80% after proton, atomic oxygen and simulated space debris (penetration) irradiation, respectively. The coupling irradiation of the first two factors resulted in a decrease of 26.93%, while the combined effect of all the three factors led to a reduction of 63.19%. Similarly, the fused silica substrates exhibited the same pattern of laser damage performance degradation. Notably, the study employed high-precision fixed-point in situ measurement techniques to track in detail the microstructural changes, surface roughness and optical-thermal absorption intensity before and after proton and atomic oxygen irradiation at the same location, thus providing a more accurate and comprehensive analysis of the damage mechanisms. In addition, simulations were conducted to quantitatively analyze the transmission trajectories and concentration distribution lines of protons and atomic oxygen incident at specific angles into the target material. 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For the high-reflection film samples, the damage thresholds decreased by 15.38%, 13.12% and 46.80% after proton, atomic oxygen and simulated space debris (penetration) irradiation, respectively. The coupling irradiation of the first two factors resulted in a decrease of 26.93%, while the combined effect of all the three factors led to a reduction of 63.19%. Similarly, the fused silica substrates exhibited the same pattern of laser damage performance degradation. Notably, the study employed high-precision fixed-point in situ measurement techniques to track in detail the microstructural changes, surface roughness and optical-thermal absorption intensity before and after proton and atomic oxygen irradiation at the same location, thus providing a more accurate and comprehensive analysis of the damage mechanisms. In addition, simulations were conducted to quantitatively analyze the transmission trajectories and concentration distribution lines of protons and atomic oxygen incident at specific angles into the target material. The research findings contribute to elucidating the laser damage performance degradation mechanism of transmissive elements in near-Earth space environments and provide technical support for the development of high-damage-threshold optical components resistant to space radiation.</abstract><cop>Cambridge, UK</cop><pub>Cambridge University Press</pub><doi>10.1017/hpl.2024.28</doi><tpages>11</tpages><orcidid>https://orcid.org/0009-0004-5619-7305</orcidid><orcidid>https://orcid.org/0000-0003-1188-4588</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Aerospace environments Atomic oxygen Charged particles Cosmic rays coupling effects Damage patterns Energy Experiments Extraterrestrial radiation Fused silica In situ measurement Laser damage laser-induced damage thresholds Lasers Microscopy Optical components Optics Performance degradation Proton damage Proton irradiation Radar systems Radiation damage Radiation tolerance Satellites Silicon dioxide Space debris space environments Substrates Surface roughness Temperature Thermal absorption Thermal cycling Thin films Thresholds Ultraviolet radiation Yield point |
title | The influence of space environmental factors on the laser-induced damage thresholds in optical components |
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