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Systems evaluation of thermal bus conceptsThermal bus concepts, to provide a centralized thermal utility for large, multihundred kilowatt space platforms, were studied and the results are summarized. Concepts were generated, defined, and screened for inclusion in system level thermal bus trades. Parametric trade studies were conducted in order to define the operational envelope, performance, and physical characteristics of each. Two concepts were selected as offering the most promise for thermal bus development. All of four concepts involved two phase flow in order to meet the required isothermal nature of the thermal bus. Two of the concepts employ a mechanical means to circulate the working fluid, a liquid pump in one case and a vapor compressor in another. Another concept utilizes direct osmosis as the driving force of the thermal bus. The fourth concept was a high capacity monogroove heat pipe. After preliminary sizing and screening, three of these concepts were selected to carry into the trade studies. The monogroove heat pipe concept was deemed unsuitable for further consideration because of its heat transport limitations. One additional concept utilizing capillary forces to drive the working fluid was added. Parametric system level trade studies were performed. Sizing and weight calculations were performed for thermal bus sizes ranging from 5 to 350 kW and operating temperatures in the range of 4 to 120 C. System level considerations such as heat rejection and electrical power penalties and interface temperature losses were included in the weight calculations.
Document ID
19830004880
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stalmach, D. D.
(Vought Corp. Dallas, TX, United States)
Date Acquired
September 4, 2013
Publication Date
February 9, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
REPT-2-53200/2R-53050
NAS 1.26:167774
NASA-CR-167774
Report Number: REPT-2-53200/2R-53050
Report Number: NAS 1.26:167774
Report Number: NASA-CR-167774
Accession Number
83N13151
Funding Number(s)
CONTRACT_GRANT: NAS9-16321
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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