JWST lightweight mirror TRL-6 results

被引:0
|
作者
Stahl, H. Philip [1 ]
机构
[1] NASA, George C Marshall Space Flight Ctr, Huntsville, AL 35812 USA
来源
2007 IEEE AEROSPACE CONFERENCE, VOLS 1-9 | 2007年
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中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Mirror technology for a Primary Mirror Segment Assembly (PMSA) is a system of components: reflective coating; polished optical surface; mirror substrate; actuators, mechanisms and flexures; and reaction structure. The functional purpose of a PMSA is to survive launch, deploy and align itself to form a 25 square meter collecting area 6.5 meter diameter primary mirror with a 131 nm rms wavefront error at temperatures < 50K and provide stable optical performance for the anticipated thermal environment. At the inception of JWST in 1996, such a capability was at a Technology Readiness Level (TRL) of 3. A highly successful technology development program was initiated including the Sub-scale Beryllium Mirror Demonstrator (SBMD) and Advanced Mirror System Demonstrator (AMSD) projects. These projects along with flight program activities have matured mirror technology for JWST to TRL-6. A directly traceable prototype (and in some cases the flight hardware itself) has been built, tested and operated in a relevant environment.(12).
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收藏
页码:1637 / 1648
页数:12
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