We investigate how different root boundary conditions for Omega booms affect the two primary requirements: small stowed volume along with high bending stiffness in the deployed configuration. For each boundary condition two finite element models are developed using the Abaqus software. The first model simulates the coiling process and is intended to get insights into the mechanics of coiling and to retrieve the shape of the transition region between the boom coiled and extended configuration which is used in the second model for computation of the bending stiffness. A specific boom design has been chosen and a physical prototype has been built.
Published January 2024
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Root Boundary Conditions for Omega Deployable Booms
Abstract
Copyright and License
© 2024 by Flavia Palmeri, Susanna Laurenzi, Sergio Pellegrino. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
Acknowledgement
Financial support form the PhD programme in Aeronautical and Space Engineering at the University of Rome LaSapienza is appreciatively recognized.
Support from the Space Solar Power Project at Caltech, USA is gratefully acknowledged
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Additional details
- Sapienza University of Rome
- California Institute of Technology
- Space Solar Power Project
- Caltech groups
- GALCIT, Space Solar Power Project
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2024-0849