The cost and leadtime associated with beryllium has forced the MDA and other defense agencies to look for alternative
materials with similar structural and thermal properties. The use of carbon-carbon material, specifically in optical
components has been demonstrated analytically in prior SBIR work at San Diego Composites. Carbon-carbon material
was chosen for its low in-plane and through-thickness CTE (athermal design), high specific stiffness, near-zero
coefficient of moisture expansion, availability of material (specifically c-c honeycomb for lightweight substrates), and
compatibility with silicon monoxide (SiO) and silicon dioxide (SiO2) coatings. Subsequent development work has
produced shaped carbon-carbon sandwich substrates which have been ground, polished, coated and figured using
traditional optical processing. Further development has also been done on machined monolithic carbon-carbon mirror
substrates which have also been processed using standard optical finishing techniques.
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