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Structural Benchmark Creep Testing for the Advanced Stirling Convertor Heater HeadThe National Aeronautics and Space Administration (NASA) has identified the high efficiency Advanced Stirling Radioisotope Generator (ASRG) as a candidate power source for use on long duration Science missions such as lunar applications, Mars rovers, and deep space missions. For the inherent long life times required, a structurally significant design limit for the heater head component of the ASRG Advanced Stirling Convertor (ASC) is creep deformation induced at low stress levels and high temperatures. Demonstrating proof of adequate margins on creep deformation and rupture for the operating conditions and the MarM-247 material of construction is a challenge that the NASA Glenn Research Center is addressing. The combined analytical and experimental program ensures integrity and high reliability of the heater head for its 17-year design life. The life assessment approach starts with an extensive series of uniaxial creep tests on thin MarM-247 specimens that comprise the same chemistry, microstructure, and heat treatment processing as the heater head itself. This effort addresses a scarcity of openly available creep properties for the material as well as for the virtual absence of understanding of the effect on creep properties due to very thin walls, fine grains, low stress levels, and high-temperature fabrication steps. The approach continues with a considerable analytical effort, both deterministically to evaluate the median creep life using nonlinear finite element analysis, and probabilistically to calculate the heater head s reliability to a higher degree. Finally, the approach includes a substantial structural benchmark creep testing activity to calibrate and validate the analytical work. This last element provides high fidelity testing of prototypical heater head test articles; the testing includes the relevant material issues and the essential multiaxial stress state, and applies prototypical and accelerated temperature profiles for timely results in a highly controlled laboratory environment. This paper focuses on the last element and presents a preliminary methodology for creep rate prediction, the experimental methods, test challenges, and results from benchmark testing of a trial MarM-247 heater head test article. The results compare favorably with the analytical strain predictions. A description of other test findings is provided, and recommendations for future test procedures are suggested. The manuscript concludes with describing the potential impact of the heater head creep life assessment and benchmark testing effort on the ASC program.
Document ID
20090004420
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Krause, David L.
(NASA Glenn Research Center Cleveland, OH, United States)
Kalluri, Sreeramesh
(Ohio Aerospace Inst. Brook Park, OH, United States)
Bowman, Randy R.
(NASA Glenn Research Center Cleveland, OH, United States)
Shah, Ashwin R.
(Sest, Inc. Middleburgh Heights, OH, United States)
Date Acquired
August 24, 2013
Publication Date
November 1, 2008
Subject Category
Metals And Metallic Materials
Report/Patent Number
AIAA-2008-5774
NASA/TM-2008-215435
Report Number: AIAA-2008-5774
Report Number: NASA/TM-2008-215435
Meeting Information
Meeting: Sixth International Energy Conversion Engineering Conference (IECEC)
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2008
End Date: July 30, 2008
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 138494.04.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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