28 August 1998 Cryogenic performance of a passive lightweight mirror
Author Affiliations +
Advanced spaceborne optical system currently under consideration, such as the Next Generation Space Telescope, will require the use of large UV segmented mirrors that can perform at cryogenic temperatures. The mirrors must be rugged, low risk, reliable, and capable of surviving launch. A design approach that utilizes passive segments in order to meet the optical system design requirements at cryogenic temperatures offers significant advantages in weight, performance, and reliability. A comparison of passive mirror designs using alternate mirror materials and the results of prototype testing at cryogenic temperature will be presented.
© (1998) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Peter A. Jones, Peter A. Jones, Donald A. Gildner, Donald A. Gildner, "Cryogenic performance of a passive lightweight mirror", Proc. SPIE 3356, Space Telescopes and Instruments V, (28 August 1998); doi: 10.1117/12.324445; https://doi.org/10.1117/12.324445


Polishability of CERAFORM silicon carbide
Proceedings of SPIE (November 10 1996)
Cesic: manufacturing study for next generation telescopes
Proceedings of SPIE (September 23 2004)
Protected silver coatings for low scatter SiC and SiC Si...
Proceedings of SPIE (December 11 2003)
Surface modification of SiC mirror by IARE method
Proceedings of SPIE (February 17 2011)

Back to Top