Spacecraft Thermal Modeling Using the Thermal Synthesizer System 961377
TSS is an integrated thermal analysis program. Using examples from the Space Station buildup sequence and the STS72 Shuttle mission, the TSS analysis process was compared with the standard process~from model building through temperature calculation and the display of results. TSS is shown to be computationally efficient in comparison to another program, TRASYS, that is commonly used for radiation analysis.
Citation: Fogerson, P., Welch, M., and Lepore, J., "Spacecraft Thermal Modeling Using the Thermal Synthesizer System," SAE Technical Paper 961377, 1996, https://doi.org/10.4271/961377. Download Citation
Author(s):
P. E. Fogerson, M. J. Welch, J. M. Lepore
Affiliated:
Hernandez Engineering, Lockheed Martin Engineering and Science Services
Pages: 8
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Spacecraft
Radiation
Simulation and modeling
SAE MOBILUS
Subscribers can view annotate, and download all of SAE's content.
Learn More »