Nacer E. Chahat;Edward Gonzales;Emmanuel Decrossas;Amy Stevens;Matthew Keyawa;Pablo S. Narvaez
{"title":"EMI-EMC Qualification of the NASA SWOT Mission Using High Fidelity Modeling","authors":"Nacer E. Chahat;Edward Gonzales;Emmanuel Decrossas;Amy Stevens;Matthew Keyawa;Pablo S. Narvaez","doi":"10.1109/JMW.2024.3522819","DOIUrl":null,"url":null,"abstract":"Surface Water and Ocean Topography (SWOT) is a complex satellite with multiple high-power transmitters and highly sensitive receivers. A pivotal feature is the Ka-band interferometer, operating at 2000 Watts, which significantly amplifies the satellite's qualification challenges. Additionally, the utilization of an X-band low-gain antenna for high data rate communication necessitates meticulous characterization and early-stage mitigation strategies to prevent interference with nearby instruments. Throughout the spacecraft's development lifecycle, meticulous attention was devoted to high-fidelity RF coupling to validate the compatibility between all instruments and preempt potential late-stage setbacks. This paper provides a comprehensive overview of the rigorous modeling and testing methodologies employed to ascertain the satellite's self-compatibility, ensuring mission success and reliability.","PeriodicalId":93296,"journal":{"name":"IEEE journal of microwaves","volume":"5 1","pages":"116-129"},"PeriodicalIF":6.9000,"publicationDate":"2025-01-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=10841827","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE journal of microwaves","FirstCategoryId":"1085","ListUrlMain":"https://ieeexplore.ieee.org/document/10841827/","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, ELECTRICAL & ELECTRONIC","Score":null,"Total":0}
引用次数: 0
Abstract
Surface Water and Ocean Topography (SWOT) is a complex satellite with multiple high-power transmitters and highly sensitive receivers. A pivotal feature is the Ka-band interferometer, operating at 2000 Watts, which significantly amplifies the satellite's qualification challenges. Additionally, the utilization of an X-band low-gain antenna for high data rate communication necessitates meticulous characterization and early-stage mitigation strategies to prevent interference with nearby instruments. Throughout the spacecraft's development lifecycle, meticulous attention was devoted to high-fidelity RF coupling to validate the compatibility between all instruments and preempt potential late-stage setbacks. This paper provides a comprehensive overview of the rigorous modeling and testing methodologies employed to ascertain the satellite's self-compatibility, ensuring mission success and reliability.