Published January 2023 | Version public
Book Section - Chapter

Buckling Analysis of a Ladder Deployable Structure Supporting a Prestressed Film

Abstract

Controlling the deflection and distortion of lightweight space structures is crucial for their function in space. In this paper, we consider the distortion of a ladder structure when being connected to a film using prestressed kirigami springs. The ladder structure is made with longitudinal CFRP Triangular Rollable and Collapsible (TRAC) booms braced by battens in the transverse direction due to prestress. This paper shows that the distortion is the result of the global buckling of the ladder structure. Then, the design space of the ladder structure has been explored to study the effects of design variables on the magnitude of shape distortion.

Additional Information

© 2023 by the American Institute of Aeronautics and Astronautics, Inc.

Additional details

Identifiers

Eprint ID
120473
Resolver ID
CaltechAUTHORS:20230327-902885000.22

Related works

Dates

Created
2023-03-30
Created from EPrint's datestamp field
Updated
2023-03-30
Created from EPrint's last_modified field

Caltech Custom Metadata

Caltech groups
GALCIT
Other Numbering System Name
AIAA Paper
Other Numbering System Identifier
2023-0366