1. NASA SP-8007 – buckling of thin-walled circular cylinders;Weingarten;NASA Space Veh Des Criteria – Struct,1965
2. Developing the next generation shell buckling design factors and technologies;Hilburger;AIAA Proc,2012
3. E.S. Agency, ESA studies future of Europe’s launch services, 25 July 2012. [accessed 12.03.13].
4. Hühne C, Rolfes R, Tessmer J. A new approach for robust design of composite cylindrical shells under axial compression, In: Proceedings of the international ESA conference. Nordwijk; 2005.
5. Hilburger MW, Nemeth MP, Starnes Jr. JH. Shell buckling design criteria based on manufacturing imperfection signatures, NASA, Report TM-2004-212659. 2004.