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Proceedings Paper

Ultralightweight active mirror technology at the University of Arizona
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Paper Abstract

Lightweight mirrors for space can be made using a thin flexible substrate for the optical surface and a rigid lightweight frame with actuators for support. The accuracy of the optical surface is actively maintained by adjusting the actuators using feedback from wavefront measurements. The University of Arizona is now in the final stages of fabricating two such mirrors. A 2-m NGST Mirror System Demonstrator, with an areal density of 13 kg/m2, is being built for NASA and will be tested at cryogenic temperatures. A 50 cm development mirror, with an areal density of only 5 kg/m2, is also being fabricated. This paper discusses the fabrication processes involved with both of these mirrors.

Paper Details

Date Published: 6 March 2001
PDF: 12 pages
Proc. SPIE 4198, Optomechanical Engineering 2000, (6 March 2001); doi: 10.1117/12.417346
Show Author Affiliations
James H. Burge, Optical Sciences Ctr./Univ. of Arizona and Steward Observatory/Univ. of Arizona (United States)
Dave Baiocchi, Optical Sciences Ctr./Univ. of Arizona (United States)
Brian Cuerden, Steward Observatory/Univ. of Arizona (United States)


Published in SPIE Proceedings Vol. 4198:
Optomechanical Engineering 2000
Mark A. Kahan, Editor(s)

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