1. 1Tibert G. "Deployable Tensegrity Structures for Space Applications", Ph.D. dissertation,Royal Institute of Technology, Stockholm, Sweden, 2002.
2. SMAP Observatory configuration, from concept to preliminary design
3. 5HarrisCooperation,"UnfurlableAntennaSolutions".Fromwebsite:http://www.harris.com/.[cited1April2012]