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Condensing Heat Exchangers as Main Components in LSS for Manned Spaceflight Nord-Micro

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Petter, Friedrich, author.
Conference Name:
International Conference On Environmental Systems (1990-07-09 : Williamsburg, Virginia, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1990
Summary:
Condensing heat exchangers are used for the thermal and humidity control within spaceflight LSS. Heat loads are transferred to a coolant loop, and humidity is removed by condensation and separation from the air flow.For minimum mass and volume at a maximum of effectiveness, adaptable plate-fin configurations are superior. Efficient separation of the condensate under zero-g conditions is achieved by enhancement of wettability of condenser surfaces with a hydrophilic coating, and the drain-off through a so-called slurper section.Exemplary, the Hermes ECLSS condensing heat exchanger and the EVA sublimator unit are presented. The advanced design comprises a new type of hydrophilic coating and several constructional details, resulting in a significant mass reduction
Notes:
Vendor supplied data
Publisher Number:
901284
Access Restriction:
Restricted for use by site license

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