System Aspects for Humidity Removal under Zero Gravity

2000-01-2312

07/10/2000

Event
International Conference On Environmental Systems
Authors Abstract
Content
The Columbus Orbital Facility (COLUMBUS) is the main European contribution to the ISS. Its Temperature and Humidity Control (THC) subsystem consists of the Condensing Heat Exchanger and Filter Assembly (CHXFA), the Condensate Water Separator Assembly (CWSA) and the Cabin Temperature Control Unit (CTCU).
The paper provides a description of the THC subsystem and its equipment focusing on the humidity removal function which has shown to be the major design challenge. Design solutions have been realised by optimising all equipment of the THC with respect to its system needs.
Test results both on equipment and on THC subsystem level are presented demonstrating that the humidity removal performance is adequate to meet the system requirements in the wide operational range of COLUMBUS.
Meta TagsDetails
DOI
https://doi.org/10.4271/2000-01-2312
Pages
7
Citation
Eicher, L., Hauser, G., Müller, R., Rose, S. et al., "System Aspects for Humidity Removal under Zero Gravity," SAE Technical Paper 2000-01-2312, 2000, https://doi.org/10.4271/2000-01-2312.
Additional Details
Publisher
Published
Jul 10, 2000
Product Code
2000-01-2312
Content Type
Technical Paper
Language
English