Published September 2017
| public
Book Section - Chapter
Ultra-Thin Composite Deployable Booms
- Creators
- Leclerc, Christophe
-
Pellegrino, Sergio
Chicago
An error occurred while generating the citation.
Abstract
Ultra-thin TRAC booms have many applications for spacecraft structures due to their very efficient packaging. A manufacturing process is proposed for composite TRAC booms with a total flange thickness of 71 μm. The mechanical behavior in both bending and torsion is studied through experiments.
Additional Information
© 2017 HafenCity University Hamburg & International Association of Shell & Spatial Structures (IASS).Additional details
- Eprint ID
- 99818
- Resolver ID
- CaltechAUTHORS:20191112-155802266
- Created
-
2019-11-13Created from EPrint's datestamp field
- Updated
-
2019-11-13Created from EPrint's last_modified field
- Caltech groups
- Space Solar Power Project, GALCIT