1 |
http://www.jaxa.jp/projects/sat/ikaros/index_e.html.
|
2 |
http://reseau.echelon.free.fr/reseau.echelon/satellites.htm.
|
3 |
http://www.globalsecurity.org/space/systems/trumpet.htm.
|
4 |
http://www.globalsecurity.org/space/systems/vortex2.htm.
|
5 |
http://www.daviddarling.info/encyclopedia/C/Chalet_Vortex.html.
|
6 |
http://space.skyrocket.de/doc_sdat/mercury.htm.
|
7 |
http://www.jaxa.jp/projects/sat/ets8/index_e.html.
|
8 |
http://www.dailywireless.org/2010/11/19/satellite-with-328-ft-antenna-to-launch/.
|
9 |
Guest S D and Pellegrino S. A new concept for solid surface deployable antennas. Acta, Astronautica, 1996, 38(2): 103-113.
DOI
ScienceOn
|
10 |
You Z. and Pellegrino S. Study of the folding and deployment aspects of a collapsible rib tensioned surface (CRTS) Antenna reflector [R]. London: Department of Engineering, University of Cambridge, 1994.
|
11 |
Tibert A.G. and Pellegrino S. Deployable tensegrity reflectors for small satellites [J]. Journal of Spacecraft and Rockets, 2002, 39(5): 701-709.
DOI
ScienceOn
|
12 |
Tibert A G., Deployable tensegrity structures for space applications [D]. Stockholm: Department of Mechanics, Royal Institute of Technology, 2002.
|