|
BEACON eSpace at Jet Propulsion Laboratory >
JPL Technical Report Server >
JPL TRS 1992+ >
Please use this identifier to cite or link to this item:
http://hdl.handle.net/2014/38006
|
| Title: | Lightweight shape memory self-deployable structures for Gossamer applications |
| Authors: | Sokolowski, Witold |
| Keywords: | Gossamer applications self-deployable ultra-lightweight spacecraft |
| Issue Date: | Apr-2004 |
| Publisher: | Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004. |
| Citation: | 45th AIAA/ASME Structures, Structural Dynamic and Materials Conference, Palm Springs, CA, April 19-22, 2004 |
| Abstract: | Currently, existing approaches for producing large, ultra-lightweight, deployable structures in space typically rely upon electro-mechanical mechanisms and mechanically expandable that are heavy, not stowage volume efficient, expensive and complex. Therefore, one of the major efforts at NASA and DoD has been to develop expandable structures characterized by low mass and small launch volume. As a result, space inflatable structures have emerged 9-10 years ago. |
| URI: | http://hdl.handle.net/2014/38006 |
| Appears in Collections: | JPL TRS 1992+
|
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.
|