Folding and Deployment of Closed Cross-Section Dual-Matrix Composite Booms-Reference-Cited by-同舟云学术

Folding and Deployment of Closed Cross-Section Dual-Matrix Composite Booms

Published:2016-01-01 Issue: Volume: Page:
ISSN:
Container-title:3rd AIAA Spacecraft Structures Conference
language:
Short-container-title:

Author:

Sakovsky Maria¹,Pellegrino Sergio¹,Mallikarachchi H.M.Y.C.²

Affiliation:

1. California Institute of Technology

2. University of Moratuwa

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0970

Reference13 articles.

1. 2Northrop Grumman. STEM Products and Programs. http://www.northropgrumman.com/BusinessVentures/ AstroAerospace/Products/Documents/pageDocs/STEM Hardware Programs.pdf, 2015.

2. Folding of fiber composites with a hyperelastic matrix

3. 5T. W. Murphey, T. Meink, and. M. M. Mikulas. Some micromechanics considerations of the folding of rigidizable composite materials. 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA 2001-1418.

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