Simulation of Deployment Process with Large Deflections for Coiled Flexible Shells Based on Prestress Initialization Method

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For coiled flexible shells, theoretical formulas of calculating the stress distribution are derived and applied to initialize the prestressed status of the shells before deploying. Following the prestress initialization, dynamic simulation of elastic and elasto-plastic deployment processes with large deflections of the shells is conducted by explicit time integration. It is shown that the simulation based on prestress initialization method is feasible and efficient. Comparing the deforming process and the energy history of the elastic deployment with that of the elasto-plastic deployment, the effects of plasticity are embodied as slowing the deployment process down and speeding the kinetic energy dissipation up, while making the shell unable to return to its original configuration, and keep more residual strain energy. A primary approach to decrease the effects of plasticity is improving the initial prestressed status of the coiled flexible shells.

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82-89

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April 2012

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] S. Pellegrino: Large Retractable Appendages in Spacecraft. Journal of Spacecraft and Rockets, Vol. 32 (1995), pp.1006-1014.

DOI: 10.2514/3.26722

Google Scholar

[2] G.W. Zhao, S.S. Du and W. Wei: Space Application and Development Trend of Deployment Mechanism. In: Proceedings of the Seventh China-Japan International Conference on History of Mechanical Technology and Mechanical Design, 31 Oct. - 2 Nov. 2008, Beijing.

Google Scholar

[3] C.S. Hazelton, K.R. Gall, E.R. Abrahamson, et al: Development of a Prototype Elastic Memory Composite STEM for Large Space Structures. In: 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, 7-10 April 2003, Norfolk, Virginia, AIAA 2003-(1977).

DOI: 10.2514/6.2003-1977

Google Scholar

[4] T. Schmidt, K. Seifart, F. Burger and J. Eder: In Orbit Bonding (IOB) of Long Deployable Structures. In: Proceedings of the 10th European Space Mechanisms and Tribology Symposium, 24-26 Sept. 2003, Paris.

Google Scholar

[5] K. Higuchi, K. Watanabe, A. Watanabe, et al: Design and Evaluation of an Ultra-light Extendible Mast as an Inflatable Structure. In: 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 1-4 May 2006, Newport, Rhode Island, AIAA 2006-1809.

DOI: 10.2514/6.2006-1809

Google Scholar

[6] F. Rehnmark, M. Pryor, B. Holmes, et al: Development of a Deployable Nonmetallic Boom for Reconfigurable Systems of Small Spacecraft. In: 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 23-26 April 2007, Honolulu, Hawaii, AIAA 2007-2184.

DOI: 10.2514/6.2007-2184

Google Scholar

[7] K.A. Seffen and S. Pellegrino: Deployment Dynamics of Tape Springs. Proceedings of the Royal Society of London A: Mathematical, Physical and Engineering Sciences, Vol. 455 (1999), pp.1003-1048.

DOI: 10.1098/rspa.1999.0347

Google Scholar

[8] J.H. Ding, K.C. Xian, X. Han, et al: Parallel Computing for Simulation of Stowing and Deployment Process of Space Lenticular Boom Mechanism. Journal of Astronautics, Vol. 32 (2011), pp.676-682.

Google Scholar

[9] E. Breitbach, C. Sickinger and L. Herbeck: Apparatus Including a Boom to Be Compressed and Rolled up. U.S. Patent 6843029B2 (2005).

Google Scholar

[10] C. Sickinger, L. Herbeck and E. Breitbach: Structural Engineering on Deployable CFRP Booms for a Solar Propelled Sailcraft. Acta Astronautica, Vol. 58 (2006), pp.185-196.

DOI: 10.1016/j.actaastro.2005.09.011

Google Scholar

[11] E. Kebadze, S.D. Guest and S. Pellegrino: Bistable Prestressed Shell Structures. International Journal of solids and structures, Vol. 41 (2004), pp.2801-2820.

DOI: 10.1016/j.ijsolstr.2004.01.028

Google Scholar