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Advanced Stirling Convertor Dual Convertor Controller Testing at NASA Glenn Research Center in the Radioisotope Power Systems System Integration LaboratoryNASA Glenn Research Center (GRC) developed a non-nuclear representation of a Radioisotope Power System (RPS) consisting of a pair of Advanced Stirling Convertors (ASC), a Dual Convertor Controller (DCC) EM (engineering model) 2 & 3, and associated support equipment, which were tested in the Radioisotope Power Systems System Integration Laboratory (RSIL). The DCC was designed by the Johns Hopkins University/Applied Physics Laboratory (JHU/APL) to actively control a pair of Advanced Stirling Convertors (ASC). The first phase of testing included a Dual Advanced Stirling Convertor Simulator (DASCS) which was developed by JHU/APL and simulates the operation and electrical behavior of a pair of ASC's in real time via a combination of hardware and software. RSIL provides insight into the electrical interactions between a representative radioisotope power generator, its associated control schemes, and realistic electric system loads. The first phase of integration testing included the following spacecraft bus configurations: capacitive, battery, and supercapacitor. A load profile, created based on data from several missions, tested the RPS and RSIL ability to maintain operation during load demands above and below the power provided by the RPS. The integration testing also confirmed the DCC's ability to disconnect from the spacecraft when the bus voltage dipped below 22 V or exceeded 36 V. Once operation was verified with the DASCS, the tests were repeated with actual operating ASC's. The goal of this integration testing was to verify operation of the DCC when connected to a spacecraft and to verify the functionality of the newly designed RSIL. The results of these tests are presented in this paper.
Document ID
20150021861
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Dugala, Gina M.
(NASA Glenn Research Center Cleveland, OH United States)
Taylor, Linda M.
(NASA Glenn Research Center Cleveland, OH United States)
Bell, Mark E.
(Vantage Partners, LLC Brook Park, OH, United States)
Dolce, James L.
(Vantage Partners, LLC Brook Park, OH, United States)
Fraeman, Martin
(Johns Hopkins Univ. Laurel, MD, United States)
Frankford, David P.
(Johns Hopkins Univ. Laurel, MD, United States)
Date Acquired
November 25, 2015
Publication Date
July 27, 2015
Subject Category
Energy Production And Conversion
Nuclear Physics
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN24658
Meeting Information
Meeting: AIAA Propulsion & Energy Forum 2015
Location: Orlando, FL
Country: United States
Start Date: July 27, 2015
End Date: July 29, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNC12BA01B
WBS: WBS 138494.04.18.01.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
systems integration
controllers
Stirling cycle
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