Buckling of Ultralight Ladder-type Coilable Space Structures
- Creators
- Royer, Fabien
-
Pellegrino, Sergio
Abstract
We analyse the buckling and post-buckling behavior of ultralight ladder-type coilable structures for space solar power applications. The structures are composed of thin-shell longitudinal elements connected by thin rods, which can be flattened and packaged efficiently. Rather than relying on an eigenvalue based analysis, this paper presents an alternative approach to thin-shell buckling based on recent work on the stability of cylindrical and spherical shells. The stability of ladder-type structures loaded by normal pressure is studied using a probe that locally displaces the structure and a stability landscape for the structure is plotted. This landscape plot gives insight into the structure's buckling, post-buckling, and sensitivity to disturbances.
Additional Information
© 2020 American Institute of Aeronautics and Astronautics. Published Online: 5 Jan 2020.Additional details
- Eprint ID
- 100663
- Resolver ID
- CaltechAUTHORS:20200113-083856811
- Created
-
2020-01-13Created from EPrint's datestamp field
- Updated
-
2021-11-16Created from EPrint's last_modified field
- Caltech groups
- GALCIT
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2020-1437