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Liquid belt radiator design studyThe Liquid Belt Radiator (LBR) is an advanced concept developed to meet the needs of anticipated future space missions. A previous study documented the advantages of this concept as a lightweight, easily deployable alternative to present day space heat rejection systems. The technical efforts associated with this study concentrate on refining the concept of the LBR as well as examining the issues of belt dynamics and potential application of the LBR to intermediate and high temperature heat rejection applications. A low temperature point design developed in previous work is updated assuming the use of diffusion pump oil, Santovac-6, as the heat transfer media. Additional analytical and design effort is directed toward determining the impact of interface heat exchanger, fluid bath sealing, and belt drive mechanism designs on system performance and mass. The updated design supports the earlier result by indicating a significant reduction in system specific system mass as compared to heat pipe or pumped fluid radiator concepts currently under consideration (1.3 kg/sq m versus 5 kg/sq m).
Document ID
19860006789
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Teagan, W. P.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Fitzgerald, K. F.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-174901
NAS 1.26:174901
Report Number: NASA-CR-174901
Report Number: NAS 1.26:174901
Accession Number
86N16259
Funding Number(s)
CONTRACT_GRANT: NAS3-23889
PROJECT: RTOP 506-55-82A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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