D. Scaccabarozzi, B. Saggin, Christian Pagliara, Marianna Magni, M. Tarabini, F. Esposito, C. Molfese, F. Cortecchia, F. Cozzolino, G. Dolnikov, I. Kuznetsov, A. Lyash, A. Zakharov
{"title":"火星颗粒分析仪的热机械设计","authors":"D. Scaccabarozzi, B. Saggin, Christian Pagliara, Marianna Magni, M. Tarabini, F. Esposito, C. Molfese, F. Cortecchia, F. Cozzolino, G. Dolnikov, I. Kuznetsov, A. Lyash, A. Zakharov","doi":"10.1109/METROAEROSPACE.2017.7999571","DOIUrl":null,"url":null,"abstract":"Airborne dust monitoring is crucial to characterize Martian atmosphere' thermal structure, balance and dynamics. In order to achieve this objective, the MicroMED instrument has been preliminary selected to join the Dust Suite payload within the ExoMars 2020 mission. The particle analyzer is mainly developed to characterize the dust on Mars but, the instrument is suitable to be mounted on different landers or rovers thanks to the limited mass budget and size. In this study, thermo-mechanical design of the instrument has been reported proving resistance and proper dynamic behavior for the expected mechanical environment.","PeriodicalId":229414,"journal":{"name":"2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2017-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":"{\"title\":\"Thermo-mechanical design of a particle analyzer for Mars\",\"authors\":\"D. Scaccabarozzi, B. Saggin, Christian Pagliara, Marianna Magni, M. Tarabini, F. Esposito, C. Molfese, F. Cortecchia, F. Cozzolino, G. Dolnikov, I. Kuznetsov, A. Lyash, A. Zakharov\",\"doi\":\"10.1109/METROAEROSPACE.2017.7999571\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Airborne dust monitoring is crucial to characterize Martian atmosphere' thermal structure, balance and dynamics. In order to achieve this objective, the MicroMED instrument has been preliminary selected to join the Dust Suite payload within the ExoMars 2020 mission. The particle analyzer is mainly developed to characterize the dust on Mars but, the instrument is suitable to be mounted on different landers or rovers thanks to the limited mass budget and size. In this study, thermo-mechanical design of the instrument has been reported proving resistance and proper dynamic behavior for the expected mechanical environment.\",\"PeriodicalId\":229414,\"journal\":{\"name\":\"2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2017-06-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"4\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/METROAEROSPACE.2017.7999571\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/METROAEROSPACE.2017.7999571","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Thermo-mechanical design of a particle analyzer for Mars
Airborne dust monitoring is crucial to characterize Martian atmosphere' thermal structure, balance and dynamics. In order to achieve this objective, the MicroMED instrument has been preliminary selected to join the Dust Suite payload within the ExoMars 2020 mission. The particle analyzer is mainly developed to characterize the dust on Mars but, the instrument is suitable to be mounted on different landers or rovers thanks to the limited mass budget and size. In this study, thermo-mechanical design of the instrument has been reported proving resistance and proper dynamic behavior for the expected mechanical environment.
求助内容：
应助结果提醒方式：
京公网安备 11010802042870号
