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Thermal Modeling Method Improvements for SAGE III on ISSThe Stratospheric Aerosol and Gas Experiment III (SAGE III) instrument is the fifth in a series of instruments developed for monitoring aerosols and gaseous constituents in the stratosphere and troposphere. SAGE III will be delivered to the International Space Station (ISS) via the SpaceX Dragon vehicle. A detailed thermal model of the SAGE III payload, which consists of multiple subsystems, has been developed in Thermal Desktop (TD). Many innovative analysis methods have been used in developing this model; these will be described in the paper. This paper builds on a paper presented at TFAWS 2013, which described some of the initial developments of efficient methods for SAGE III. The current paper describes additional improvements that have been made since that time. To expedite the correlation of the model to thermal vacuum (TVAC) testing, the chambers and GSE for both TVAC chambers at Langley used to test the payload were incorporated within the thermal model. This allowed the runs of TVAC predictions and correlations to be run within the flight model, thus eliminating the need for separate models for TVAC. In one TVAC test, radiant lamps were used which necessitated shooting rays from the lamps, and running in both solar and IR wavebands. A new Dragon model was incorporated which entailed a change in orientation; that change was made using an assembly, so that any potential additional new Dragon orbits could be added in the future without modification of the model. The Earth orbit parameters such as albedo and Earth infrared flux were incorporated as time-varying values that change over the course of the orbit; despite being required in one of the ISS documents, this had not been done before by any previous payload. All parameters such as initial temperature, heater voltage, and location of the payload are defined based on the case definition. For one component, testing was performed in both air and vacuum; incorporating the air convection in a submodel that was only built for the in-air cases allowed correlation of all testing to be done in a single model. These modeling improvements and more will be described and illustrated in the paper.
Document ID
20160006467
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Liles, Kaitlin
(NASA Langley Research Center Hampton, VA, United States)
Amundsen, Ruth
(NASA Langley Research Center Hampton, VA, United States)
Davis, Warren
(NASA Langley Research Center Hampton, VA, United States)
McLeod, Shawn
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Date Acquired
May 20, 2016
Publication Date
August 3, 2015
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-21362
Report Number: NF1676L-21362
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop (TFAWS 2015)
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)
WBS: WBS 857865.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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