Development of Fabric-Based Materials for Space Applications

Item

Title
Development of Fabric-Based Materials for Space Applications
Description
This project was designed to produce new and improved coated fibrous structure materials for rigidizable expanded structures for future aerospace uses. Woven fiberglas is coated with polymeric compositions designed to retain flexibility until rigidization is required. Two techniques involving removal of part of the coating (normally a plasticizer) are evaluated and found satisfactory for producing a rigid structure. Inflatable structures are used to demonstrate the methods. A third procedure for rigidization is outlined from a theoretical viewpoint only. The investigation is restricted to continuous-filament glass yarn and coating compounds based on polyvinyl chloride and polyurethane polymers. The effects of yarns, weaves, and coating composition are investigated with respect to their rigidization capability. Criteria used to determine the relative merit of a coated fabric matrix are buckling strength under compression loading and modification of the standard stiffness test for plastics. Relative rates of rigidization are measured for several candidate materials
Date
1963
Date Issued
1963-01
Publisher
Wright-Patterson Air Force Base, OH : Directorate of Materials & Processes, Aeronautical Systems Division, Air Force Systems Command
DoD Project
7320 - Fibrous Materials for Decelerators and Structures
DoD Task
None Given
Abstract
This project was designed to produce new and improved coated fibrous structure materials for rigidizable expanded structures for future aerospace uses. Woven fiberglas is coated with polymeric compositions designed to retain flexibility until rigidization is required. Two techniques involving removal of part of the coating (normally a plasticizer) are evaluated and found satisfactory for producing a rigid structure. Inflatable structures are used to demonstrate the methods. A third procedure for rigidization is outlined from a theoretical viewpoint only.
The investigation is restricted to continuous-filament glass yarn and coating compounds based on polyvinyl chloride and polyurethane polymers. The effects of yarns, weaves, and coating composition are investigated with respect to their rigidization capability. Criteria used to determine the relative merit of a coated fabric matrix are buckling strength under compression loading and modification of the standard stiffness test for plastics. Relative rates of rigidization are measured for several candidate materials
Index Abstract
Contrails only
Laboratory
Directorate of Materials & Processes
Distribution Conflict
No
Distribution Classification
1
Identifier
AD0299030
DTIC Record Exists
No
Report Availability
Full text available
Extent
18
Corporate Author
Westinghouse Electric Corporation
Report Number
ASD TDR 62-964, p. 291-307
Provenance
Lockheed Martin Missiles & Fire Control
Creator
Gosnell, C. N.
Hawthorn, A. T.
Type
article
Relation
This paper was presented at the Directorate of Materials and Processes "Symposium on Fibrous Materials" held in Dayton, Ohio, on 16-17 October 1962
Format
1 online resource (18 pages)

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Items with "Has Part: Development of Fabric-Based Materials for Space Applications"
Title Class
Symposium on Fibrous Materials