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Application of Simulated Reactivity Feedback in Nonnuclear Testing of a Direct-Drive Gas-Cooled ReactorNonnuclear testing can be a valuable tool in the development of an in-space nuclear power or propulsion system. In a nonnuclear test facility, electric heaters are used to simulate heat from nuclear fuel. Standard testing allows one to fully assess thermal, heat transfer, and stress related attributes of a given system but fails to demonstrate the dynamic response that would be present in an integrated, fueled reactor system. The integration of thermal hydraulic hardware tests with simulated neutronic response provides a bridge between electrically heated testing and full nuclear testing. By implementing a neutronic response model to simulate the dynamic response that would be expected in a fueled reactor system, one can better understand system integration issues, characterize integrated system response times and response and response characteristics, and assess potential design improvements with a relatively small fiscal investment. Initial system dynamic response testing was demonstrated on the integrated SAFE 100a heat pipe cooled, electrically heated reactor and heat exchanger hardware. This Technical Memorandum discusses the status of the planned dynamic test methodology for implementation in the direct-drive gas-cooled reactor testing and assesses the additional instrumentation needed to implement high-fidelity dynamic testing.
Document ID
20070035891
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Bragg-Sitton, S. M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Webster, K. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
June 1, 2007
Subject Category
Engineering (General)
Report/Patent Number
NASA/TM-2007-214959
M-1188
Report Number: NASA/TM-2007-214959
Report Number: M-1188
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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