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ISS-CREAM Thermal and Fluid System Design and AnalysisThermal and Fluids Analysis Workshop (TFAWS), Silver Spring MD NCTS 21070-15. The ISS-CREAM (Cosmic Ray Energetics And Mass for the International Space Station) payload is being developed by an international team and will provide significant cosmic ray characterization over a long time frame. Cold fluid provided by the ISS Exposed Facility (EF) is the primary means of cooling for 5 science instruments and over 7 electronics boxes. Thermal fluid integrated design and analysis was performed for CREAM using a Thermal Desktop model. This presentation will provide some specific design and modeling examples from the fluid cooling system, complex SCD (Silicon Charge Detector) and calorimeter hardware, and integrated payload and ISS level modeling. Features of Thermal Desktop such as CAD simplification, meshing of complex hardware, External References (Xrefs), and FloCAD modeling will be discussed.
Document ID
20150020904
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Thorpe, Rosemary S.
(Bastion Technologies, Inc. United States)
Date Acquired
November 6, 2015
Publication Date
August 3, 2015
Subject Category
Instrumentation And Photography
Fluid Mechanics And Thermodynamics
Report/Patent Number
GSFC-E-DAA-TN25002
Report Number: GSFC-E-DAA-TN25002
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop (TFAWS)
Location: Silver Spring, MD
Country: United States
Start Date: August 3, 2015
End Date: August 7, 2015
Sponsors: NASA Goddard Space Flight Center
Funding Number(s)
CONTRACT_GRANT: NNG12CR29C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Thermal analysis
0000
Temperature Control
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