NASA NTRS · 20130013416
Light Weight Silicon Mirrors for Space Instrumentation
Abstract
Each mirror is a monolithic structure from a single crystal of silicon. The mirrors are light weighted after the optical surface is ground and polished. Mirrors made during the initial phase of this work were typically 1/50 lambda or better (RMS at 633 n m)
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Bly, Vincent T., Hill, Peter C., Hagopian, John G., Strojay, Carl R., Miller, Timothy. 2012-08-12. Light Weight Silicon Mirrors for Space Instrumentation. https://ntrs.nasa.gov/citations/20130013416
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