Paper
27 April 1988 The Flexure Assembly Design For The SIRTF One-Meter Primary Mirror
R. M. Richard, D Vukobratovich, M. Cho, L. W. Pollard, R. K. Melugin
Author Affiliations +
Abstract
A titanium flexure assembly for the Space Infrared Telescope Facility (SIRTF) 1-m primary mirror has been designed to accommodate (1) the cryogenic cool-down effect on the optical performance of the mirror, (2) the shuttle launch-load envi:onment, and (3) the support-baseplate manufacturing tolerances. Numerous iterations involving a multi-dimensional design space search led to an assembly design that provides the stiffness and strength in the vertical (optical axis) and tangential directions to accommodate launch loads, but is compliant radially to accommodate cryogenic cool down. A "folded back" titanium flexure system was required because of the differential thermal contraction of the aluminum telescope baseplate support and the fused-silica mirror. This unique and innovative flexure assembly represents a totally passive mechanism for accommodating the design launch loads, cryogenic cool down, and out-of-plane baseplate effects.
© (1988) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
R. M. Richard, D Vukobratovich, M. Cho, L. W. Pollard, and R. K. Melugin "The Flexure Assembly Design For The SIRTF One-Meter Primary Mirror", Proc. SPIE 0973, Cryogenic Optical Systems and Instruments III, (27 April 1988); https://doi.org/10.1117/12.948343
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Cited by 1 scholarly publication.
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KEYWORDS
Mirrors

Cryogenics

Titanium

Space telescopes

Aluminum

Optical cryogenics

Assembly tolerances

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