The activated heat source concept for space power applications

dc.contributor.advisorPeddicord, K. L.
dc.contributor.committeeMemberAlred, J. W.
dc.contributor.committeeMemberSaylak, D.
dc.contributor.committeeMemberSchlapper, G. A.
dc.creatorThomas, James Kelly
dc.date.accessioned2020-09-02T20:12:18Z
dc.date.available2020-09-02T20:12:18Z
dc.date.issued1992
dc.descriptionTypescript (photocopy).en
dc.description.abstractOne of the most reliable and commonly selected options for low levels of electrical power production (few kW[e] or less) in space is the radioisotope thermoelectric generator (RTG), which employs plutonium-238 (238Pu) as a heat source and thermoelectrics for conversion of thermal to electrical energy. These systems have been successfully applied to a wide range of missions and the associated thermal management, energy conversion and structural technologies have reached a high level of maturity. Another system employing 238Pu as the thermal energy source, but targeted for moderately higher power levels (up to 10 kW[e]), is the dynamic isotope power system (DIPS). Space reactors are under development to meet higher power requirements. However, each of these systems have drawbacks that might be overcome through development and application of activated heat source (AHS) technology. The AHS concept involves replacement of the 238Pu heat source in an RTG or DIPS with a material that is either non-radioactive or has a relatively low specific activity. The AHS material would be activated by a space reactor after launch to generate a thermal energy source. The thermal management, power conversion, and structural technologies developed for RTG and DIPS are transferable to the AHS concept. The AHS concept would eliminate or reduce the radiological hazards associated with the launch of plutonium-bearing power systems while preserving much of the investment made to date in the associated technologies, and increase the available supply of heat source material. The AHS concept would also increase the utilization of space reactor power systems. The objective of this study was to demonstrate the basic feasibility of the AHS concept. Candidate source nuclides were identified based on nuclear property requirements, and the basic materials performance and availability of these nuclides were investigated...en
dc.format.digitalOriginreformatted digitalen
dc.format.extentxii, 190 leavesen
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.identifier.oclc27843778
dc.identifier.urihttps://hdl.handle.net/1969.1/DISSERTATIONS-1293015
dc.language.isoeng
dc.publisher.digitalTexas A&M University. Libraries
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/
dc.subjectMajor nuclear engineeringen
dc.subject.classification1992 Dissertation T458
dc.subject.lcshSpace vehiclesen
dc.subject.lcshNuclear power plantsen
dc.subject.lcshRadionuclide generatorsen
dc.titleThe activated heat source concept for space power applicationsen
dc.typeThesisen
dc.type.genredissertationsen
dc.type.materialtexten
thesis.degree.grantorTexas A&M Universityen
thesis.degree.nameDoctor of Philosophyen
thesis.degree.namePh. Den

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