28 September 2011 JWST NIRCam flight mirror assemblies
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The Near Infrared Camera (NIRCam) instrument for NASA's James Webb Space Telescope (JWST) has an optical prescription which includes numerous fold mirror assemblies. The instrument will operate at 35K after experiencing launch loads at ~293K. The optic mounts must accommodate all associated thermal and mechanical stresses, plus maintain exceptional optical quality during operation. Lockheed Martin Space Systems Company (LMSSC) conceived, designed, analyzed, assembled, tested, and integrated the mirror assemblies for the NIRCam instrument. This paper covers the design, analysis, assembly, and test of two of the instruments key fold mirrors.
© (2011) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Paul V. Mammini, Paul V. Mammini, Howard C. Holmes, Howard C. Holmes, Lynn Huff, Lynn Huff, Mike S. Jacoby, Mike S. Jacoby, Frank Lopez, Frank Lopez, } "JWST NIRCam flight mirror assemblies", Proc. SPIE 8150, Cryogenic Optical Systems and Instruments XIII, 81500D (28 September 2011); doi: 10.1117/12.896470; https://doi.org/10.1117/12.896470


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