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Consolidation of A Sodium Heat Pipe and Stirling Engine for Fission Surface PowerThe Consolidated Heat Pipe (CHP) is a new design in which a sodium heat pipe is welded directly to the hot end of the Stirling engine to deliver thermal power more efficiently. The new integrated interface aims to reduce the large temperature drop (about 120 °C) that was measured across the bolted clamp joint between the Stirling engine and the heat pipes during the Kilopower Reactor Using Stirling TechnologY (KRUSTY) test from 2018.

Initial testing and characterization of the CHP was performed in ambient air at the NASA Glenn Research Center (GRC). In the test, the heat pipe evaporator section was heated with a tube furnace. The thermal power was then transported to the Stirling engine integrated with a linear alternator that produced electrical power. The CHP has been tested at a hot end temperature ranging from 600 °C - 800 °C and a variety of other Stirling engine parameters (cold end temperature, piston amplitude and pressure). The results show that the temperature drop between the Stirling engine and the heat pipe has been reduced to 2°C - 4 °C. An overall temperature drop of 20 °C – 60 °C was also noted within the heat pipe depending on the combination of parameters mentioned above. Overall, it has been shown that the new Consolidated Heat Pipe design significantly improved the thermal interface to the Stirling engine.
Document ID
20230010646
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Greeta J. Thaikattil
(Glenn Research Center Cleveland, Ohio, United States)
James L. Sanzi
(HX5 (United States) Fort Walton Beach, Florida, United States)
Daniel Goodell
(Glenn Research Center Cleveland, Ohio, United States)
Christopher Barth
(Glenn Research Center Cleveland, Ohio, United States)
Marc Gibson
(Gibson Engineering)
Date Acquired
July 20, 2023
Subject Category
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: Thermal Fluids Analysis Workshop (TFAWS)
Location: College Park, MD
Country: US
Start Date: August 21, 2023
End Date: August 25, 2023
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 658133.04.01.22.01.02
CONTRACT_GRANT: 80GRC020D0003
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Consolidated
Integrated
Heat Pipe
Stirling Engine
Fission
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