Integration of Thermal and Environmental Control Systems During Space Station Freedom Early Assembly Phase 921259
An overview of Space Station Freedom Thermal Control System (TCS) and Environmental Control and Life Support System (ECLSS) integration is presented for Stages 2-6. Particular attention is given to issues associated with integrating five distinct, functioning spacecraft with hardware not specifically designed for intermediate stages. Areas specifically addressed include integrated ECLSS temperature and humidity control performance, thermal load balancing, performance and verification requirements, interface verification procedures, TCS activation sequence, resource allocation and Space Shuttle integration.
Citation: Di Pietro, D. and Tandler, J., "Integration of Thermal and Environmental Control Systems During Space Station Freedom Early Assembly Phase," SAE Technical Paper 921259, 1992, https://doi.org/10.4271/921259. Download Citation
Author(s):
David A. Di Pietro, John J. Tandler
Pages: 16
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Life support systems
Spacecraft
Control systems
SAE MOBILUS
Subscribers can view annotate, and download all of SAE's content.
Learn More »
