| contributor author | Arup K. Maji | |
| contributor author | Peter Wegner | |
| contributor author | Refugio Rochin | |
| date accessioned | 2017-05-08T21:16:10Z | |
| date available | 2017-05-08T21:16:10Z | |
| date copyright | April 2004 | |
| date issued | 2004 | |
| identifier other | %28asce%290893-1321%282004%2917%3A2%2883%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/45003 | |
| description abstract | The ability to create lightweight mirrors that can maintain surface accuracy is a major technical challenge for future space telescopes. Processing-induced errors and surface errors due to temperature excursions and gravity sag (zero gravity in space) make it impossible to correct the surface of thin mirror face-sheets by conventional point actuators. The challenges are compounded by the requirements for mirrors to have adequate stiffness for pointing accuracy. An experimental and analytical study was conducted to explore the feasibility of correcting the shape of lightweight (≈1 kg/m | |
| publisher | American Society of Civil Engineers | |
| title | Surface Actuation of Lightweight Mirrors with Shape Memory Alloy | |
| type | Journal Paper | |
| journal volume | 17 | |
| journal issue | 2 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2004)17:2(83) | |
| tree | Journal of Aerospace Engineering:;2004:;Volume ( 017 ):;issue: 002 | |
| contenttype | Fulltext | |
