Title :
JWST Lightweight Mirror TRL-6 Results
Author_Institution :
NASAMSFCXD-30, Huntsville
Abstract :
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.
Keywords :
aerospace instrumentation; astronomical telescopes; infrared astronomy; mirrors; Advanced Mirror System Demonstrator; JWST lightweight mirror TRL-6; PMSA; Sub-scale Beryllium Mirror Demonstrator; Technology Readiness Level; actuators; anticipated thermal environment; flight program activities; mirror substrate; mirror technology; polished optical surface; primary mirror segment assembly; reaction structure; reflective coating; Actuators; Assembly systems; Coatings; Hardware; Mirrors; Optical devices; Optical surface waves; Prototypes; Temperature; Testing;
Conference_Titel :
Aerospace Conference, 2007 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
1-4244-0524-6
Electronic_ISBN :
1095-323X
DOI :
10.1109/AERO.2007.353006