Paper
17 September 1998 Cryogenic optical performance of the Cassini composite infrared spectrometer (CIRS) flight telescope
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Abstract
The Cassini Composite InfraRed Spectrometer half-mirror diameter beryllium flight telescope's optical performance was tested at the instrument operating temperature of 170 Kelvin. The telescope components were designed at Goddard Space Flight Center (GSFC) but fabricated out-of-house and then assembled, aligned, and tested upon receipt at GSFC. A 24-inch aperture cryogenic test facility utilizing a 1024 X 1024 CCD array was developed at GSFC specifically for this test. The telescope's image quality (measured as encircled energy), boresight stability and focus stability were measured. The gold coated beryllium design exceeded the cold image performance requirement of 80% encircled energy within a 460 micron diameter cycle.
© (1998) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Patricia A. Losch, James J. Lyons III, and John G. Hagopian "Cryogenic optical performance of the Cassini composite infrared spectrometer (CIRS) flight telescope", Proc. SPIE 3435, Cryogenic Optical Systems and Instruments VIII, (17 September 1998); https://doi.org/10.1117/12.323742
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Cited by 1 scholarly publication.
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KEYWORDS
Telescopes

Mirrors

Beryllium

Space telescopes

Collimation

Cryogenics

Infrared spectroscopy

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