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Optimal structural design of the Airborne Infrared Imager 254202
Gimbal mechanism for cryogenic alignment of 1meter diameter optics 254203
Modal analysis tests on the supporting structure of the secondary mirror of the Large Binocular
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adhesive alignment alloy aluminum analysis angle angular applications arcseconds aspheric axial azimuthal bearing Beryllium birefringence cantilever beam coefficient components configuration coupling loss cryogenic deflection detector determine diameter diamond machining diaphragm diaphragm flexure diffraction displacement effects electroless nickel equations error fabrication fiber film finite element analysis finite element model focus frequency FRFs fundamental frequency fused silica gimbal gimbal assembly inches instrument interferometer laser length lens lightweight linear load material maximum measurement mechanical method micrometer modal module non-linearities optical axis optical bench optical elements optical fibre optical surface optical system optimized optomechanical PACE parameters parasitic motions performance plasma etching plating polishing position precision predicted primary mirror radial range resin retainer ring rotation sensor shown in Figure silicon carbide simple flexure stage spid SPIE stability stiffness stress structure substrate Table telescope temperature thermal expansion thickness waveguide wavelength x-ray