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Stirling Technology Development at NASA GRCThe Department of Energy, Stirling Technology Company (STC), and NASA Glenn Research Center (NASA Glenn) are developing a free-piston Stirling convertor for a high-efficiency Stirling Radioisotope Generator (SRG) for NASA Space Science missions. The SRG is being developed for multimission use, including providing electric power for unmanned Mars rovers and deep space missions. NASA Glenn is conducting an in-house technology project to assist in developing the convertor for space qualification and mission implementation. Recent testing, of 55-We Technology Demonstration Convertors (TDC's) built by STC includes mapping, of a second pair of TDC's, single TDC testing, and TDC electromagnetic interference and electromagnetic compatibility characterization on a nonmagnetic test stand. Launch environment tests of a single TDC without its pressure vessel to better understand the convertor internal structural dynamics and of dual-opposed TDC's with several engineering mounting structures with different natural frequencies have recently been completed. A preliminary life assessment has been completed for the TDC heater head, and creep testing of the IN718 material to be used for the flight convertors is underway. Long-term magnet aging tests are continuing to characterize any potential aging in the strength or demagnetization resistance of the magnets used in the linear alternator (LA). Evaluations are now beginning on key organic materials used in the LA and piston/rod surface coatings. NASA Glenn is also conducting finite element analyses for the LA, in part to look at the demagnetization margin on the permanent magnets. The world's first known integrated test of a dynamic power system with electric propulsion was achieved at NASA Glenn when a Hall-effect thruster was successfully operated with a free-piston Stirling power source. Cleveland State University is developing a multidimensional Stirling computational fluid dynamics code to significantly improve Stirling loss predictions and assist in identifying convertor areas for further improvements. This paper will update the status and results for these efforts.
Document ID
20020038545
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Authors
Thieme, Lanny G.
(NASA Glenn Research Center Cleveland, OH United States)
Schreiber, Jeffrey G.
(NASA Glenn Research Center Cleveland, OH United States)
Mason, Lee S.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:211315/REV1
NASA/TM-2001-211315/REV1
E-13119/REV1
Report Number: NAS 1.15:211315/REV1
Report Number: NASA/TM-2001-211315/REV1
Report Number: E-13119/REV1
Meeting Information
Meeting: Space Technology and Applications International Forum
Location: Albuquerque, NM
Country: United States
Start Date: February 3, 2002
End Date: February 7, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 783-82-00
PROJECT: RTOP 755-A4-14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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