Space Station Integrated Temperature and Humidity Control Analysis Using SINDA/FLUINT

961350

07/01/1996

Event
International Conference On Environmental Systems
Authors Abstract
Content
The National Aeronautics and Space Administration (NASA) International Space Station contains several thermal/fluid systems. The Integrated Thermal Analysis (ITA) Group at McDonnell Douglas Aerospace/Houston (under Task Order to the Prime Contractor) performs the integrated thermal analyses for thermal verification of various Space Station configurations. A SINDA/FLUINT model of the Temperature and Humidity Control system (THC) was constructed in support of this effort.
This paper presents the modeling strategy used in creating a THC model with SINDA/FLUINT. Also presented, are a sample of results from the THC model as it was used in analyzing Space Station Flight 6A.
Meta TagsDetails
DOI
https://doi.org/10.4271/961350
Pages
8
Citation
Augustine, J., "Space Station Integrated Temperature and Humidity Control Analysis Using SINDA/FLUINT," SAE Technical Paper 961350, 1996, https://doi.org/10.4271/961350.
Additional Details
Publisher
Published
Jul 1, 1996
Product Code
961350
Content Type
Technical Paper
Language
English