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Multi-Physics Based Thermo-Well Fatigue Design Tool In this study, mathematical-based models for fatigue life were developed for Resistance Temperature Detectors (RTDs)/thermo-wells in high-pressure, cryogenic flow environments. A literature review that identified bench-scale stainless steel fatigue data at cryogenic temperatures that can be used to validate fatigue life mathematical models was pursued. Developing the ability to predict the fatigue life of RTDs/thermo-wells in high-pressure, cryogenic flow environments, especially liquid oxygen (LOX), will lead to a lower incidence of RTD damage and failure during propulsion test activities. During this performance period, the project was transitioned to a computational RTD/thermos-well fatigue modeling effort rather than the previously proposed experimental fatigue testing in FY19 since the computational modeling approach will provide a better fundamental understanding of fatigue behavior at cryogenic temperatures prior to pursuing potentially costly experimental tests. Due to COVID-19 issues impairing access to some needed university partnerships, tools and lab facilities, FY20efforts are continuing into FY21 and will be reported upon in greater detail in the FY21 report
Document ID
20210013098
Acquisition Source
Stennis Space Center
Document Type
Other - FY20 CIF Report
Authors
Harry Ryan
(Stennis Space Center Bay Saint Louis, Mississippi, United States)
Date Acquired
April 2, 2021
Publication Date
April 5, 2021
Subject Category
Propellants And Fuels
Funding Number(s)
CONTRACT_GRANT: 295670.01.20.64.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
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