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Cryogenic Etalon
Program Description
Michigan Aerospace Corporation designed, fabricated and tested a spaceflight-qualified tunable Fabry-Perot etalon. This
device is operated at 77 Kelvin from 7 - 11 microns. Tuning is accomplished via this use of ferroelectric single crystals
and provides a range of travel of approximately 20 microns at operating temperature. Zinc Selenide was used for all
transmitting elements. Titanium (Ti-6Al-5V Grade 5) was used for the etalon mount due to its low density, high strength,
and coefficient of thermal expansion. The etalon was delivered to NASA’s Langley Reseach Center in July of 2004.”
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Cryogenic
Etalon Requirements and Parameters
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Parameter
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Desired
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Minimum
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Design Projected
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Wavelength
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9-12um
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-
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-
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Gap
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-
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-
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3.7mm
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Finesse
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20
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12
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19.3
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Transmission
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11%
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8%
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8.10%
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Resolution
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0.07 cm-1
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6.32 Angstroms at 9.5um
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6.32 Angstroms at 9.5um
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Reflectivity
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0.8
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0.6-0.9
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0.85
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Dynamic Range
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25um
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5um
(1/2 wavelength)
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20.5
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Free Spectral Range
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Maximize
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-
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12.2nm
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Thermal analysis picture of etalon during design |
Two views of completed etalon
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