International Space Station Alpha Internal Thermal Control System Coldplate Development

941492

06/01/1994

Event
International Conference On Environmental Systems
Authors Abstract
Content
A family of ten coldplates has been developed. These form an integral part of the International Space Station Alpha internal thermal control system (ITCS) and provide necessary cooling for electronics and experimental equipment. These coldplates are robust single-passage, single-pass, plate-fin heat exchangers. They provide surface-mounted equipment cooling with a minimum coolant pressure drop, minimum weight, and maximum service life at an economical cost. The ten coldplates vary in size, thermal performance, and equipment mounting configuration.
This paper describes the design and performance of each coldplate. Data from performance tests and performance derivations based on the test data are presented. These data are presented in a form suitable for use in the design of equipment applications.
Meta TagsDetails
DOI
https://doi.org/10.4271/941492
Pages
9
Citation
Mickelson, E., and Buchmann, O., "International Space Station Alpha Internal Thermal Control System Coldplate Development," SAE Technical Paper 941492, 1994, https://doi.org/10.4271/941492.
Additional Details
Publisher
Published
Jun 1, 1994
Product Code
941492
Content Type
Technical Paper
Language
English