Published January 5, 2020
| public
Book Section - Chapter
Ultralight Deployable Space Structure Prototype
Chicago
Abstract
We present a lab demonstration of the packaging and deployment of an ultralight space structure prototype composed of thin shell longerons and battens. The prototype is integrated with a thin polyimide membrane which serves as mass representative of multi-functional elements that could be integrated into this type of deployable, such as integrated power collection and wireless transmission tiles for space solar power. A deployment mechanism using actively controlled pressure to package and deploy this structure ensuring its integrity is described. The deployable structure and deployment mechanism designs are scalable to 60 m X 60 m structures. The structure's mass scaling to larger sizes is described.
Additional Information
© 2020 American Institute of Aeronautics and Astronautics. Published Online: 5 Jan 2020.Additional details
- Eprint ID
- 100655
- Resolver ID
- CaltechAUTHORS:20200113-080052698
- 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
- 2020-0692