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NASA NTRS · 19900043841

Composite deformable mirror

Abstract

A mathematical model for a spherical hexagon mirror is described along with the model verifications. A flat hexagon epoxy mirror with aluminum core is used in test procedures in addition to a flat aluminum honeycomb mirror. Deformable reflector concepts are discussed and piezoelectric actuators are analyzed. The concept of a deformable mirror can be used to improve the overall RMS error of the mirror as presently designed and/or make necessary on-orbit adjustments.

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BibTeXRIS

Kuo, C. P., Wada, B. K.. 1989-01-01. Composite deformable mirror. https://ntrs.nasa.gov/citations/19900043841

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