Nonlinear Analysis of the Vega Launcher First Stage composite skirts with geometrical imperfections-Reference-Cited by-同舟云学术

Nonlinear Analysis of the Vega Launcher First Stage composite skirts with geometrical imperfections

Published:2007-04-23 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Biagi Michele¹,Perugini Pierluigi²

Affiliation:

1. CNES Centre National d'Etudes Spatiales - Launchers Directorate

2. AVIO S.p.A. Propulsione Aerospziale

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-2120

Reference18 articles.

1. 2Biagioni, M., Cutroni, M., and Pascal, P. "P80 FW SRM - New Technologies for Solid Rocket Motor - Status of Development,"40th AIAA/ASME/SAE/ASEEJoint PropulsionConference andExhibit,AIAA-2004-4220

2. 3Limam, A, Jullien, J.F., Greco, E., and Lestrat, D. "Buckling of thin-walled cylinder under axial compression and internal pressure,"International Colloquium on Bucklingof Shells Structures, on Land, inthe Sea andinthe Air,Lyon, 1991.

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3. Design and Development of Vega Solid Rocket Motors Composite Cases;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08