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Advanced Stirling receiver development program, phase 1Critical technology experiments were designed and developed to evaluate the Stirling cavity heat pipe receiver for a space solar power system. Theoretical criteria were applied to the design of a module for containing energy storage phase change material while avoiding thermal ratcheting. Zero-g drop tower tests, without phase change, were conducted to affirm that the bubble location required to avoid ratcheting could be achieved without the use of container materials that are wetted by the phase change material. A full scale module was fabricated, but not tested. A fabrication method was successfully developed for the sodium evaporator dome, with a sintered screen wick, to be used as the focal point for the receiver. Crushing of the screen during hydroforming was substantially reduced over the results of other researchers by using wax impregnation. Superheating of the sodium in the wick under average flux conditions is expected to be under 10K. A 2000K furnace which will simulate solar flux conditions for testing the evaporator dome was successfully built and tested.
Document ID
19910008139
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lurio, Charles A.
(Lockheed Sanders, Inc. Nashua, NH, United States)
Date Acquired
September 6, 2013
Publication Date
July 18, 1990
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-CR-185281
NAS 1.26:185281
Report Number: NASA-CR-185281
Report Number: NAS 1.26:185281
Accession Number
91N17452
Funding Number(s)
CONTRACT_GRANT: NAS3-25471
PROJECT: RTOP 506-41-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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