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Materials Chemistry Issues in the Development of a Single-Crystal Solar/Thermal Refractive Secondary ConcentratorA translucent crystal concentrates and transmits energy to a heat exchanger, which in turn heats a propellant gas, working gas of a dynamic power system, or a thermopile. Materials are the limiting issue in such a system. Central is the durability of the crystal, which must maintain the required chemical, physical/optical, and mechanical properties as it is heated and cooled. This report summarizes available data to date on the materials issues with this system. We focus on the current leading candidate materials, which are sapphire (Al2O3) for higher temperatures and silica (SiO2) for lower temperatures. We use data from thermochemical calculations; laboratory coupon tests with silica and sapphire; and system tests with sapphire. The required chemical properties include low-vapor pressure and interfacial stability with supporting structural materials. Optical properties such as transmittance and index of refraction must be maintained. Thermomechanical stability is a major challenge for a large, single-crystal ceramic and has been discussed in another report. In addition to the crystal, other materials in the proposed system include refractory metals (Nb, Ta, Mo, W, and Re), carbon (C), and high-temperature ceramic insulation. The major issue here is low levels of oxygen, which lead to volatile refractory metal oxides and rapid consumption of the refractory metal. Interfacial reactions between the ceramic crystal and refractory metal are also discussed. Finally, high-temperature ceramic insulating materials are also likely to be used in this system. Outgassing is a major issue for these materials. The products of outgassing are typically reactive with the refractory metals and must be minimized.
Document ID
20050180629
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Jacobson, Nathan S.
(NASA Glenn Research Center Cleveland, OH, United States)
Biering, Robert C.
(Analex Corp. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2005
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TM-2005-213625
E-15109
Funding Number(s)
WBS: WBS 22-972-30-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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