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Shuttle active thermal control system development testing. Volume 3: Modular radiator system test data correlation with thermal modelResults are presented of an analysis which compares the performance predictions of a thermal model of a multi-panel modular radiator system with thermal vacuum test data. Comparisons between measured and predicted individual panel outlet temperatures and pressure drops and system outlet temperatures have been made over the full range of heat loads, environments and plumbing arrangements expected for the shuttle radiators. Both two sided and one sided radiation have been included. The model predictions show excellent agreement with the test data for the maximum design conditions of high load and hot environment. Predictions under minimum design conditions of low load-cold environments indicate good agreement with the measured data, but evaluation of low load predictions should consider the possibility of parallel flow instabilities due to main system freezing. Performance predictions under intermediate conditions in which the majority of the flow is not in either the main or prime system are adequate although model improvements in this area may be desired. The primary modeling objective of providing an analytical technique for performance predictions of a multi-panel radiator system under the design conditions has been met.
Document ID
19740026229
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Phillips, M. A.
(LTV Aerospace Corp. Dallas, TX, United States)
Date Acquired
September 3, 2013
Publication Date
December 18, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-140269
T169-28-VOL-3
Report Number: NASA-CR-140269
Report Number: T169-28-VOL-3
Accession Number
74N34342
Funding Number(s)
CONTRACT_GRANT: NAS9-10534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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