columbus · Application of Permselective Composite Techniques for Atmosphere-Thermal Control of Emergency

Application of Permselective Composite Techniques for Atmosphere-Thermal Control of Emergency

Item

Title: Application of Permselective Composite Techniques for Atmosphere-Thermal Control of Emergency
Date: 1967
Index Abstract: Not Available
Photo Quality: Not Needed
Report Number: AMRL TR 66-224
Creator: Withey, D. J.; Glanfield, E. J.; Dohner, C. V.
Corporate Author: General Electric Company
Laboratory: Aerospace Medical Research Laboratories
Extent: 94
Identifier: AD0655089
Access Rights: Distribution of this document is unlimited
Distribution Classification: 1
Contract: AF 33(615)-2850
DoD Project: 6373
DoD Task: 637302
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: No
Abstract: The program encompasses the analysis, research, design fabrication, and testing of an exploratory laboratory model of an emergency or extravehicular space assembly using permselective membrane techniques for atmosphere control. The purpose of this effort was to develop an advanced concept which would depart from the traditional approach utilized in spacecraft design by transferring most of the atmosphere-thermal control functions from the associated hardware subsystems to the enclosing structure. A silicon rubber permselective composite incorporated into the pressure retention wall of the enclosing structure permits selective permeation of carbon dioxide, water vapor, and contaminant gases to space with minimal oxygen permeation. In addition, the use of superinsulation on the exterior surface of the structure provides passive radiant thermal control. This, in conjunction with the permselective composite material, substantially reduces the weight, volume, and power requirements of environmental control subsystems required for a manned emergency and extravehicular assembly. While the permselectivity of the silicone rubber composite was determined, the final structure was subject to a large amount of leakage. This resulted in the cancellation of the full scale test program and in redirection of the project effort to include a failure analysis to determine the cause and solution to the leakage problem.
Report Availability: Full text available
Date Issued: 1967-04
Provenance: RAF Centre of Aviation Medicine
Type: report
Format: 1 online resource

Media: AMRLTR66-224.pdf