{"title":"空间环境试验台(套):用于搭载卫星实验的适应性系统","authors":"K. Fowler, L. Frank, R.L. Williams","doi":"10.1109/IMTC.2003.1208146","DOIUrl":null,"url":null,"abstract":"This paper introduces the concept of a flexible, adaptable subsystem for satellites that provides a platform for space-based experiments. The subsystem, called a carrier, comprises mechanical, electrical/electronic, thermal, data, and software components. We have performed a number of tradeoff studies and recommend a general type of architecture for the carrier that will satisfy many requirements and accommodate the constraints of space-based experimentation.","PeriodicalId":135321,"journal":{"name":"Proceedings of the 20th IEEE Instrumentation Technology Conference (Cat. No.03CH37412)","volume":"48 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2003-05-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Space environment testbed (set): adaptable system for piggybacked satellite experiments\",\"authors\":\"K. Fowler, L. Frank, R.L. Williams\",\"doi\":\"10.1109/IMTC.2003.1208146\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper introduces the concept of a flexible, adaptable subsystem for satellites that provides a platform for space-based experiments. The subsystem, called a carrier, comprises mechanical, electrical/electronic, thermal, data, and software components. We have performed a number of tradeoff studies and recommend a general type of architecture for the carrier that will satisfy many requirements and accommodate the constraints of space-based experimentation.\",\"PeriodicalId\":135321,\"journal\":{\"name\":\"Proceedings of the 20th IEEE Instrumentation Technology Conference (Cat. No.03CH37412)\",\"volume\":\"48 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2003-05-20\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the 20th IEEE Instrumentation Technology Conference (Cat. No.03CH37412)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/IMTC.2003.1208146\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the 20th IEEE Instrumentation Technology Conference (Cat. No.03CH37412)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/IMTC.2003.1208146","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Space environment testbed (set): adaptable system for piggybacked satellite experiments
This paper introduces the concept of a flexible, adaptable subsystem for satellites that provides a platform for space-based experiments. The subsystem, called a carrier, comprises mechanical, electrical/electronic, thermal, data, and software components. We have performed a number of tradeoff studies and recommend a general type of architecture for the carrier that will satisfy many requirements and accommodate the constraints of space-based experimentation.