Nonlinear finite element model for the analysis of axisymmetric inflatable beams

Author:

Elsabbagh Adel

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference26 articles.

1. T.R. Cawsey, A deployment mechanism for the double roll-out flexible solar array on the space telescope, in: Proceedings of the 16th Aerospace Mechanisms Symposium, NASA CP-2221, 1982.

2. G. Knouse, W. Weber, NASA Mobile Satellite Program, Large Satellite Antennas and Space Technology, NASA CR-2368 part 1, 1984.

3. M. Di Capua, D.L. Akin, K. Davis, Design, development, and testing of an inflatable habitat element for NASA lunar analogue studies, in: Proceedings of the 41st International Conference on Environmental Systems, Portland, Oregon, AIAA 2011–5044.

4. S.D. Guest, Deployable Structures: Concepts and Analysis, Corpus Christi College, University of Cambridge.

5. Gossamer Spacecraft: Membrane/Inflatable Structures Technologies for Space Applications;Jenkins,2001

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