S. L. Katz, J. Likar, Chi H. Pham, Dakai Chen, Natnael J. Ahmed
{"title":"Heavy Ion Single Event Effects (SEE) results for OPA128 Electrometer Grade Operational Amplifier","authors":"S. L. Katz, J. Likar, Chi H. Pham, Dakai Chen, Natnael J. Ahmed","doi":"10.1109/NSREC45046.2021.9679341","DOIUrl":null,"url":null,"abstract":"The OPA128 is an electrometer grade operational amplifier with femtoamp bias currents [1], potentially offering better performance than other rad-hard precision op amps available today [2], [3], [4], [5], [6]. Heavy ion testing to qualify it for use on the Europa Clipper mission uncovered a destructive failure not noted in prior testing [7], [8], [9], precipitating additional testing to explore the failure and determine the part's viability for spaceflight. Testing yielded a proposed safe operating area (SOA). Non-destructive transient events were also observed and characterized for multiple applications.","PeriodicalId":340911,"journal":{"name":"2021 IEEE Nuclear and Space Radiation Effects Conference (NSREC)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2021 IEEE Nuclear and Space Radiation Effects Conference (NSREC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/NSREC45046.2021.9679341","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
The OPA128 is an electrometer grade operational amplifier with femtoamp bias currents [1], potentially offering better performance than other rad-hard precision op amps available today [2], [3], [4], [5], [6]. Heavy ion testing to qualify it for use on the Europa Clipper mission uncovered a destructive failure not noted in prior testing [7], [8], [9], precipitating additional testing to explore the failure and determine the part's viability for spaceflight. Testing yielded a proposed safe operating area (SOA). Non-destructive transient events were also observed and characterized for multiple applications.