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Comparison of dynamic isotope power systems for distributed planet surface applicationsDynamic isotope power system (DIPS) alternatives were investigated and characterized for the surface mission elements associated with a lunar base and subsequent manned Mars expedition. System designs based on two convertor types were studied. These systems were characterized parametrically and compared over the steady-state electrical output power range 0.2 to 20 kWe. Three methods of thermally integrating the heat source and the Stirling heater head were considered, depending on unit size. Figures of merit were derived from the characterizations and compared over the parametric range. Design impacts of mission environmental factors are discussed and quantitatively assessed.
Document ID
19910018964
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bents, David J.
(NASA Lewis Research Center Cleveland, OH., United States)
Mckissock, Barbara I.
(NASA Lewis Research Center Cleveland, OH., United States)
Hanlon, James C.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Schmitz, Paul C.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Rodriguez, Carlos D.
(NASA Lewis Research Center Cleveland, OH., United States)
Withrow, Colleen A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-5905
NASA-TM-4303
NAS 1.15:4303
Report Number: E-5905
Report Number: NASA-TM-4303
Report Number: NAS 1.15:4303
Accession Number
91N28278
Funding Number(s)
PROJECT: RTOP 326-81-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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