1 |
Horner, G. G. and Elliot, M. D., "A Fabrication and Development Approach for a Miura-Ori Solar Sail Model", Proc. 43rd SDM Conference, AIAA-2002-1702, Denver, CO, April 22-25, 2002.
|
2 |
Papa, A. and Pellegrino, S.,“Systematically Creased Thin-Film MembraneStructures", J. Spacecrafts and Rockets, Vol. 45,pp. 10-18, 2008.
DOI
ScienceOn
|
3 |
Hossain, N.M.A., Woo, K. and Jenkins,C.H., "Nonlinear Material Response ofSystematically Creased Membranes", Proc. of47th SDM Conference, AIAA-2006-1801, 1-4 May2006, Newport, RI.
|
4 |
우경식, "접힌자국이 있는 멤브레인의 주름 거동 연구", 한국항공우주학회지, 제 36 권 제 9호, 2008, pp. 851-858.
|
5 |
Tessler, A., Sleight, D. and Wang, J.T.,"Effective Modeling and Nonlinear ShellAnalysis of Thin Membranes ExhibitingStructural Wrinkling", J. Spacecrafts and Rockets,Vol. 42, pp. 287-298, 2005.
DOI
ScienceOn
|
6 |
Mukulas, M. M. and Adler, A., "RapidStructural Assessment Approach for SquareSolar Sails Including Edge Support Cords",Proc. 44th SDM Conf., AIAA 2003-1447, Norfolk,VA, April 7-10, 2003.
|
7 |
Miura, K., "Method of Packaging andDeployment of Large Membranes in Space",International Astronautical Federation, PaperIAF-80-A31, Tokyo, Japan, 1980.
|