Thermal Synthesizer System - An integrated approach to spacecraft thermal analysisThe Thermal Synthesizer System (TSS), which is being developed to meet the thermal analysis needs of Space Station Freedom and of the proposed Space Exploration Initiative missions, is examined. The key requirements and design goals to be met by TSS are summarized, and the software engineering and user interface design philosophy are reviewed. The basic architecture for all applications within TSS is described. An overview is given of the main features of each of the applications of TSS.
Document ID
19920039263
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Panczak, Tim (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Fried, Larry (Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Rickman, Steven (NASA Johnson Space Center Houston, TX, United States)
Welch, Mark (Lockheed Engineering and Sciences Co. Houston, TX, United States)