Concept-Development of a Structure Supported Membrane for Deployable Space Applications - From Nature to Manufacture and TestingCurrent space applications of membrane structures include large area solar power arrays, solar sails, antennas, and numerous other large aperture devices like the solar shades of the new James Webb Space Telescope. These expandable structural systems, deployed in-orbit to achieve the desired geometry, are used to collect, reflect and/or transmit electromagnetic radiation. This work, a feasibility study supporting a diploma thesis, describes the systematic process for developing a biologically inspired concept for a structure supported (integrated) membrane, that features a rip stop principle, makes self-deployment possible and is part of an ultra-light weight space application. Novel manufacturing of membrane prototypes and test results are presented for the rip-stop concepts. Test data showed that the new membrane concept has a higher tear resistance than neat film of equivalent mass.
Document ID
20120011940
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Zander, Martin (Technische Univ. Brunswick, Germany)
Belvin, W. K. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 26, 2013
Publication Date
March 30, 2012
Subject Category
Structural Mechanics
Report/Patent Number
NF1676L-14193Report Number: NF1676L-14193
Meeting Information
Meeting: European Conference on Spacecraft Structures, Materials and Environmental Testing