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Thermal expansion behavior of NiSi/NiSi sub 2

Journal Article · · Scripta Metallurgica et Materialia; (United States)
;  [1]
  1. Metals and Ceramics Div., Oak Ridge National Lab., Oak Ridge, TN (US)
This paper reports that advanced space power systems that use solar energy and Brayton or Stirling heat engines require thermal energy storage systems for continuous operation during periods of darkness. The receiver storage units, key elements in both Brayton and Stirling systems, are designed to use the latent heat of fusion of phase change materials. Energy is stored during the heating and melting of a phase change material (PCM) in the sunlit portion of the orbit. The PCM cools and freezes, thereby releasing heat to the engine, during the eclipse period of the orbit. The power systems under current consideration for near-future NASA space missions require working fluid temperatures in the 1100 to 1400 K range. The high thermal conductivity and generally low volume change on melting of alloys based on silicon make them attractive for storage of thermal energy in space power systems. However, the chemical reactivity of these materials narrows the choice of containment materials to ceramics that generally have very poor strength and crystallographic direction-dependent thermal transfer properties. For physical compatibility, the expansion of the PCM and container material must be very closely matched. Thus, the thermal expansion of NiSi/NiSi{sub 2} (a very desirable PCM) was determined.
DOE Contract Number:
AC05-84OR21400
OSTI ID:
7295739
Journal Information:
Scripta Metallurgica et Materialia; (United States), Journal Name: Scripta Metallurgica et Materialia; (United States) Vol. 26:1; ISSN SCRME; ISSN 0956-716X
Country of Publication:
United States
Language:
English