Stowage and Deployment Strength of a Rollable Composite Shell Reflector

Author:

Keil Tyler1,Banik Jeremy2

Affiliation:

1. Missouri University of Science and Technology

2. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Reference10 articles.

1. Folding of woven composite structures

2. 1 Unidirectional [deg] Surface % % % % % % Top 0.002 -0.972 0.330 -0.014 0.073 -0.073

3. Bottom 0.001 -1.882 0.728 -0.041 0.130 -0.130 Top 0.008 -0.471 0.007 -0.471 1.168 -0.003

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2. Examining Energy Dissipation of Deployable Aerospace Composites Using Matrix Viscoelasticity;Journal of Aerospace Engineering;2017-09

3. Shaping of Rollable, Singly Curved, Parabolic Shell Reflectors;Journal of Spacecraft and Rockets;2016-05

4. Large Strain Four-Point Bending of Thin Unidirectional Composites;Journal of Spacecraft and Rockets;2015-05

5. Creep Effects and Deployment Characterization of Rollable Composite Shell Reflectors;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

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