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Thermal Design and Analysis of Columbus Pressurized Modules
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English
Abstract
Thermal control design of Columbus pressurised modules has evolved throughout phases B and C0 of the program leading to the C/D proposal emission. Proposal comments by the European Space Agency (ESA), negotiation of interfaces between Space Station Freedom (SSF) partners, possible advantageous design commonalities among the attached pressurised modules and MTFF reconfiguration are ongoing activities.
This paper discusses the design solutions presented in the thermal control subsystem C/D proposal including modifications deriving from updated ESA requirements and preliminary feedback from negotiation of interfaces.
Authors
Citation
Dolce, S., Ciampolini, F., and Dodd, C., "Thermal Design and Analysis of Columbus Pressurized Modules," SAE Technical Paper 901369, 1990, https://doi.org/10.4271/901369.Also In
References
- Dolce S. Trichilo M. Berardi F. Thermal Control of Columbus Pressurised Modules 3rd European Symposium on Space Thermal Control and Life Support Systems ESTEC Noordwijk 3-6 October 1988
- Dolce S. Trichilo M. Dodd C. Active Thermal Control Design of Columbus Pressurised Modules 19th ICES Conference San Diego 24-27 July 1989