As wavefront quality demands tighten on space systems for applications such as astronomy and laser communication, mounting small optics such that the wavefront is undisturbed, positioning is adjustable and the design is producible, while surviving harsh space environments, is a continuing challenge. We designed multiple candidate flexure mounts to support small optics (up to 50 mm diameter, and over 100 grams) to survive the qualification and acceptance tests of small spacecraft and units as defined in ISO 19683 and a mounting structure which is adjustable in decenter [+/-0.5mm], tip/tilt +/-0.5deg, and piston [+/-0.25mm]. We will present design details along with measurements showing less than approximately lambda/10 wavefront contribution from the optic bonding process, along with thermal and multi-axis vibration test data showing the mounted optics survived the acceptance testing loads and are suitable for operation in a wide range of harsh environments.
In this paper we discuss the final mechanical design of the GIRMOS Cryostat. GIRMOS is an adaptive optics fed multi-object Integral-Field Spectrograph (IFS) with a parallel imaging capability and will be installed at the Gemini North Observatory. This instrument includes four identical spectrograph channels arranged symmetrically around a central optical axis which provides it with a multiplexing capability. GIRMOS has an object selection sub-assembly (OSEL) located upstream of the spectrographs which contains four motorized fold mirror assemblies that can scan the incoming light from the telescope to look at four separate sections of the sky simultaneously or can combine their efforts to look at a single larger section of the sky in a tiled mode. Each of the four individual IFS beams from the OSEL assembly is directed into the instrument Cryostat via its dedicated optical entrance window. Within the Cryostat each IFS beam moves through an anamorphic relay, an optical image slicer assembly, and eventually makes it to a spectrograph unit. In this paper, we will provide some details regarding the vacuum chamber design that houses the spectrographs, the design of the internal support structure, the opto-mechanical packaging of the IFS along with some of the thermal load mitigation techniques employed.
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