{"title":"Bayesian Reliability Analysis of the Enhanced Multimission Radioisotope Thermoelectric Generator","authors":"Chung H. Lee, Thierry Caillat, S. Pinkowski","doi":"10.2514/1.a35785","DOIUrl":null,"url":null,"abstract":"Radioisotope thermoelectric generators (RTGs) have been used as power sources for several space missions, including the multimission RTG (MMRTG) in NASA’s recent Mars Curiosity and Perseverance rovers. The enhanced MMRTG (eMMRTG) design is an MMRTG retrofitted with advanced skutterudite thermoelectric couples to improve efficiency and power output over time. The eMMRTG’s predicted reliability over the mission duration is influenced by the uncertainty in the physics parameters governing its performance. We use a Bayesian approach to account for two types of uncertainty: epistemic and aleatory. The reliability analysis has two steps: 1) uncertainty quantification from experimental data for key physics parameters, and 2) uncertainty propagation through a computational RTG life performance prediction. In particular, we use hierarchical models to separate specimen-to-specimen uncertainty and also to model the separate manufacturing batches of thermoelectric couples loaded into the eMMRTG. We use a secondary probability method to predict reliability with epistemic uncertainty intervals for the eMMRTG system at 10,000 h for which recent data are available. We show how reliability and uncertainty intervals depend on hypothetical power requirements at 10,000 h. The approach is generally applicable when experimental data and computer simulation are used to predict the reliability of a new technology.","PeriodicalId":50048,"journal":{"name":"Journal of Spacecraft and Rockets","volume":"122 8","pages":""},"PeriodicalIF":1.3000,"publicationDate":"2024-01-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Spacecraft and Rockets","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.2514/1.a35785","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0
Abstract
Radioisotope thermoelectric generators (RTGs) have been used as power sources for several space missions, including the multimission RTG (MMRTG) in NASA’s recent Mars Curiosity and Perseverance rovers. The enhanced MMRTG (eMMRTG) design is an MMRTG retrofitted with advanced skutterudite thermoelectric couples to improve efficiency and power output over time. The eMMRTG’s predicted reliability over the mission duration is influenced by the uncertainty in the physics parameters governing its performance. We use a Bayesian approach to account for two types of uncertainty: epistemic and aleatory. The reliability analysis has two steps: 1) uncertainty quantification from experimental data for key physics parameters, and 2) uncertainty propagation through a computational RTG life performance prediction. In particular, we use hierarchical models to separate specimen-to-specimen uncertainty and also to model the separate manufacturing batches of thermoelectric couples loaded into the eMMRTG. We use a secondary probability method to predict reliability with epistemic uncertainty intervals for the eMMRTG system at 10,000 h for which recent data are available. We show how reliability and uncertainty intervals depend on hypothetical power requirements at 10,000 h. The approach is generally applicable when experimental data and computer simulation are used to predict the reliability of a new technology.
期刊介绍:
This Journal, that started it all back in 1963, is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental result. The topics include aeroacoustics, aerodynamics, combustion, fundamentals of propulsion, fluid mechanics and reacting flows, fundamental aspects of the aerospace environment, hydrodynamics, lasers and associated phenomena, plasmas, research instrumentation and facilities, structural mechanics and materials, optimization, and thermomechanics and thermochemistry. Papers also are sought which review in an intensive manner the results of recent research developments on any of the topics listed above.