{"title":"The Landsat-6 satellite: an overview","authors":"E.W. Mowle, C. Dennehy","doi":"10.1109/NTC.1991.148030","DOIUrl":null,"url":null,"abstract":"Landsat 6 (L6), a remote land sensing satellite, is scheduled to be launched into a 705 km, circular, sun-synchronous orbit by a Titan-II booster in mid 1992. The L6 satellite has been designed to provide 30 m spatial resolution multispectral image data continuity via an enhanced thematic mapper (ETM) sensor which includes a panchromatic band with 15 m spatial resolution. A brief background description of the Landsat system is provided and the top-level L6 mission requirements are reviewed to identify the sensor and spacecraft bus design drivers. The L6-era combined EOSAT ground/space system configuration is highlighted. The design and operation of the high-data-rate ETM mission sensor and the major spacecraft bus subsystems are described in detail.<<ETX>>","PeriodicalId":320008,"journal":{"name":"NTC '91 - National Telesystems Conference Proceedings","volume":"24 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1991-03-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"NTC '91 - National Telesystems Conference Proceedings","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/NTC.1991.148030","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 4
Abstract
Landsat 6 (L6), a remote land sensing satellite, is scheduled to be launched into a 705 km, circular, sun-synchronous orbit by a Titan-II booster in mid 1992. The L6 satellite has been designed to provide 30 m spatial resolution multispectral image data continuity via an enhanced thematic mapper (ETM) sensor which includes a panchromatic band with 15 m spatial resolution. A brief background description of the Landsat system is provided and the top-level L6 mission requirements are reviewed to identify the sensor and spacecraft bus design drivers. The L6-era combined EOSAT ground/space system configuration is highlighted. The design and operation of the high-data-rate ETM mission sensor and the major spacecraft bus subsystems are described in detail.<>