Dehumidification Via Membrane Separation for Space-Based Applications

881037

7/1/1988

Authors
Abstract
Content
This paper describes the development of a membrane-based dehumidification process for space-based applications, such as spacecraft cabins and extra-vehicular-activity (EVA) space suits. Results presented are from 1) screening tests conducted to determine the efficacy of various membranes to separate water vapor from air, and 2) parametric and long-term tests of membranes operated at conditions that simulate the range of environmental conditions (e.g., temperature and relative humidity [RH]) expected in the planned space station. Also included in this paper is a discussion of preliminary designs of membrane-based dehumidification processes for the space station and EVA space suits. These designs result in compact and energy-efficient systems that offer significant advantages over conventional dehumidification processes.
Meta TagsDetails
DOI
https://doi.org/10.4271/881037
Pages
20
Citation
Gienger, J., Ray, R., and Chullen, C., "Dehumidification Via Membrane Separation for Space-Based Applications," SAE Technical Paper 881037, 1988, https://doi.org/10.4271/881037.
Additional Details
Publisher
Published
7/1/1988
Product Code
881037
Content Type
Technical Paper
Language
English