Sadeq Malakooti , Stephanie L. Vivod , Kim K. de Groh , Jessica L. Cashman , Mary Ann B. Meador , DanielA. Scheiman , Jonathan A. Salem , Sylvie F. Crowell , Linda S. McCorkle
{"title":"Space environment exposure effects on polyimide aerogels","authors":"Sadeq Malakooti , Stephanie L. Vivod , Kim K. de Groh , Jessica L. Cashman , Mary Ann B. Meador , DanielA. Scheiman , Jonathan A. Salem , Sylvie F. Crowell , Linda S. McCorkle","doi":"10.1016/j.polymdegradstab.2025.111398","DOIUrl":null,"url":null,"abstract":"<div><div>As part of the Materials International Space Station Experiment (MISSE) missions, polyimide aerogel samples as prepared and atomic oxygen plasma treated with bulk densities of 0.09 and 0.15 g/cm<sup>3</sup> were exposed on the exterior of the International Space Station (ISS) during MISSE-9, 12, and 15 missions for 0.77, 0.89, and 0.44-year direct space exposure times, respectively. The aerogel samples were synthesized from a combination of the diamines 1,3-bis(4-aminophenoxy)-2,2-dimethylpropane (BAPN) and 2,2′-dimethylbenzidine (DMBZ), 3,3′,4,4′-biphenyltetracarboxylic dianhydride (BPDA), and 1,3,5-triaminophenoxybenzene (TAB) as the crosslinker. At low Earth orbit (LEO), spacecraft are subjected to extreme environmental conditions such as thermal cycling, solar radiation, cosmic rays, solar wind charged particles and atomic oxygen (AO). A post-flight analysis of aerogel physical, chemical, mechanical, thermal and optical properties were performed using a series of non-destructive techniques. The polyimide aerogels exhibited a notably higher AO erosion yield compared to nonporous Kapton H or HN polyimides, attributed to their order of magnitude lower bulk density and much higher surface area. Yet, the post-flight characterizations reveal no significant degradation in material properties. For example, in terms of material’s structural integrity, the post-flight Young’s moduli at both low and high densities were not statistically changed. Similar observations were obtained for thermal and optical properties in terms of changes in the materials’ thermal conductivity and solar absorptance. The aerogel flight samples with pre-flight surface treatments using atomic oxygen plasma showed a higher susceptibility to the LEO environment compared to as-prepared aerogel flight samples. Despite their high AO erosion yield, this study shows that polyimide aerogels maintain remarkable stability throughout extended space missions and explorations and therefore can be considered as a space-rated material.</div></div>","PeriodicalId":406,"journal":{"name":"Polymer Degradation and Stability","volume":"239 ","pages":"Article 111398"},"PeriodicalIF":6.3000,"publicationDate":"2025-04-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Polymer Degradation and Stability","FirstCategoryId":"92","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0141391025002277","RegionNum":2,"RegionCategory":"化学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"POLYMER SCIENCE","Score":null,"Total":0}
引用次数: 0
Abstract
As part of the Materials International Space Station Experiment (MISSE) missions, polyimide aerogel samples as prepared and atomic oxygen plasma treated with bulk densities of 0.09 and 0.15 g/cm3 were exposed on the exterior of the International Space Station (ISS) during MISSE-9, 12, and 15 missions for 0.77, 0.89, and 0.44-year direct space exposure times, respectively. The aerogel samples were synthesized from a combination of the diamines 1,3-bis(4-aminophenoxy)-2,2-dimethylpropane (BAPN) and 2,2′-dimethylbenzidine (DMBZ), 3,3′,4,4′-biphenyltetracarboxylic dianhydride (BPDA), and 1,3,5-triaminophenoxybenzene (TAB) as the crosslinker. At low Earth orbit (LEO), spacecraft are subjected to extreme environmental conditions such as thermal cycling, solar radiation, cosmic rays, solar wind charged particles and atomic oxygen (AO). A post-flight analysis of aerogel physical, chemical, mechanical, thermal and optical properties were performed using a series of non-destructive techniques. The polyimide aerogels exhibited a notably higher AO erosion yield compared to nonporous Kapton H or HN polyimides, attributed to their order of magnitude lower bulk density and much higher surface area. Yet, the post-flight characterizations reveal no significant degradation in material properties. For example, in terms of material’s structural integrity, the post-flight Young’s moduli at both low and high densities were not statistically changed. Similar observations were obtained for thermal and optical properties in terms of changes in the materials’ thermal conductivity and solar absorptance. The aerogel flight samples with pre-flight surface treatments using atomic oxygen plasma showed a higher susceptibility to the LEO environment compared to as-prepared aerogel flight samples. Despite their high AO erosion yield, this study shows that polyimide aerogels maintain remarkable stability throughout extended space missions and explorations and therefore can be considered as a space-rated material.
期刊介绍:
Polymer Degradation and Stability deals with the degradation reactions and their control which are a major preoccupation of practitioners of the many and diverse aspects of modern polymer technology.
Deteriorative reactions occur during processing, when polymers are subjected to heat, oxygen and mechanical stress, and during the useful life of the materials when oxygen and sunlight are the most important degradative agencies. In more specialised applications, degradation may be induced by high energy radiation, ozone, atmospheric pollutants, mechanical stress, biological action, hydrolysis and many other influences. The mechanisms of these reactions and stabilisation processes must be understood if the technology and application of polymers are to continue to advance. The reporting of investigations of this kind is therefore a major function of this journal.
However there are also new developments in polymer technology in which degradation processes find positive applications. For example, photodegradable plastics are now available, the recycling of polymeric products will become increasingly important, degradation and combustion studies are involved in the definition of the fire hazards which are associated with polymeric materials and the microelectronics industry is vitally dependent upon polymer degradation in the manufacture of its circuitry. Polymer properties may also be improved by processes like curing and grafting, the chemistry of which can be closely related to that which causes physical deterioration in other circumstances.