Advanced Thermal Control Technologies for European Space Station Modules

851366

07/01/1985

Event
Intersociety Conference on Environmental Systems
Authors Abstract
Content
The European space station activities are momentary concentrated on the “COLUMBUS” studies. The high heat transport capabilities, required for the COLUMBUS modules necessitate further development of “Two-Phase Flow Heat Transport” systems as well as hybrid radiator elements. Within a technology study, sponsored by ESTEC, a dedicated design for a European platform had been defined after the evaluation and analysis of the COLUMBUS platform requirements. The proposed solution will be described in detail. The design possibilities of space constructable/deployable heat pipe radiators applicable for COLUMBUS modules will be given. In addition, the growth capabilities of these concepts and maintainability aspects will be explained.
Meta TagsDetails
DOI
https://doi.org/10.4271/851366
Pages
12
Citation
Möller, P., and Kreeb, H., "Advanced Thermal Control Technologies for European Space Station Modules," SAE Technical Paper 851366, 1985, https://doi.org/10.4271/851366.
Additional Details
Publisher
Published
Jul 1, 1985
Product Code
851366
Content Type
Technical Paper
Language
English