Published January 5, 2020 | Version public
Book Section - Chapter

Buckling of Ultralight Ladder-type Coilable Space Structures

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

Identifiers

Eprint ID
100663
Resolver ID
CaltechAUTHORS:20200113-083856811

Dates

Created
2020-01-13
Created from EPrint's datestamp field
Updated
2021-11-16
Created from EPrint's last_modified field

Caltech Custom Metadata

Caltech groups
GALCIT
Other Numbering System Name
AIAA Paper
Other Numbering System Identifier
2020-1437