M. Orefice, V. Quaranta, G. Bruno, Giuseppe Martinotti, Carmine Carandente Tartaglia
{"title":"准静态载荷空间鉴定试验","authors":"M. Orefice, V. Quaranta, G. Bruno, Giuseppe Martinotti, Carmine Carandente Tartaglia","doi":"10.1109/MetroAeroSpace51421.2021.9511773","DOIUrl":null,"url":null,"abstract":"Satellites are designed and tested to withstand to static and dynamic operative loads during the launch and the ascent phase. The validation of the structural design of the satellite is generally performed by tests and/or analysis. The paper presents the static load test methods with a focus on the sine-burst quasi-static load test. A test procedure will be presented in order to overcome the main issues related to a sine-burst test. Finally test results performed on a 6U Cubesat will be discussed.","PeriodicalId":236783,"journal":{"name":"2021 IEEE 8th International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"20 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-06-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Quasi-static load space qualification test\",\"authors\":\"M. Orefice, V. Quaranta, G. Bruno, Giuseppe Martinotti, Carmine Carandente Tartaglia\",\"doi\":\"10.1109/MetroAeroSpace51421.2021.9511773\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Satellites are designed and tested to withstand to static and dynamic operative loads during the launch and the ascent phase. The validation of the structural design of the satellite is generally performed by tests and/or analysis. The paper presents the static load test methods with a focus on the sine-burst quasi-static load test. A test procedure will be presented in order to overcome the main issues related to a sine-burst test. Finally test results performed on a 6U Cubesat will be discussed.\",\"PeriodicalId\":236783,\"journal\":{\"name\":\"2021 IEEE 8th International Workshop on Metrology for AeroSpace (MetroAeroSpace)\",\"volume\":\"20 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-06-23\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2021 IEEE 8th International Workshop on Metrology for AeroSpace (MetroAeroSpace)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/MetroAeroSpace51421.2021.9511773\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2021 IEEE 8th International Workshop on Metrology for AeroSpace (MetroAeroSpace)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MetroAeroSpace51421.2021.9511773","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Satellites are designed and tested to withstand to static and dynamic operative loads during the launch and the ascent phase. The validation of the structural design of the satellite is generally performed by tests and/or analysis. The paper presents the static load test methods with a focus on the sine-burst quasi-static load test. A test procedure will be presented in order to overcome the main issues related to a sine-burst test. Finally test results performed on a 6U Cubesat will be discussed.
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