{"title":"直读微流星体探测分析仪","authors":"L. Snyder","doi":"10.1109/TA.1965.4319810","DOIUrl":null,"url":null,"abstract":"To determine the harmful effects of micrometeoroids and measure their occurrence in space, a unique detector-analyzer system has been developed for NASA Manned Spacecraft Center. The system consists of a modified ballistic pendulum for momentum measurement and appropriate arrangement of capacitive foils for velocity determination. A prototype instrument has been successfully tested in the dynamic range extending from 1 to 45 dynesec.","PeriodicalId":13050,"journal":{"name":"IEEE Transactions on Aerospace","volume":"17 1","pages":"258-263"},"PeriodicalIF":0.0000,"publicationDate":"1965-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"A Direct Reading Micrometeoroid Detector-Analyzer\",\"authors\":\"L. Snyder\",\"doi\":\"10.1109/TA.1965.4319810\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"To determine the harmful effects of micrometeoroids and measure their occurrence in space, a unique detector-analyzer system has been developed for NASA Manned Spacecraft Center. The system consists of a modified ballistic pendulum for momentum measurement and appropriate arrangement of capacitive foils for velocity determination. A prototype instrument has been successfully tested in the dynamic range extending from 1 to 45 dynesec.\",\"PeriodicalId\":13050,\"journal\":{\"name\":\"IEEE Transactions on Aerospace\",\"volume\":\"17 1\",\"pages\":\"258-263\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1965-06-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Transactions on Aerospace\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/TA.1965.4319810\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Aerospace","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/TA.1965.4319810","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
To determine the harmful effects of micrometeoroids and measure their occurrence in space, a unique detector-analyzer system has been developed for NASA Manned Spacecraft Center. The system consists of a modified ballistic pendulum for momentum measurement and appropriate arrangement of capacitive foils for velocity determination. A prototype instrument has been successfully tested in the dynamic range extending from 1 to 45 dynesec.
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