Paper
13 September 2012 Conceptual phase A design of a cryogenic shutter mechanism for the SAFARI flight instrument
Max Eigenmann, Udo J. Wehmeier, Aurèle Vuilleumier, Gabriele Messina, Michael R. Meyer
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Abstract
We present a conceptual design for a cryogenic optical mechanism for the SAFARI instrument. SAFARI is a long wavelength (34-210 micron) Imaging Fourier Transform Spectrometer (FTS) to fly as an ESA instrument on the JAXA SPICA mission projected to launch in 2021. SPICA is a large 3m class space telescope which will have an operating temperature of less than 7K. The SAFARI shutter is a single point of failure flight mechanism designed to operate in space at a temperature of 4K which meets redundancy and reliability requirements of this challenging mission. The conceptual design is part of a phase A study led by ETH Institute for Astronomy and conducted by RUAG Space AG.
© (2012) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Max Eigenmann, Udo J. Wehmeier, Aurèle Vuilleumier, Gabriele Messina, and Michael R. Meyer "Conceptual phase A design of a cryogenic shutter mechanism for the SAFARI flight instrument", Proc. SPIE 8450, Modern Technologies in Space- and Ground-based Telescopes and Instrumentation II, 84504G (13 September 2012); https://doi.org/10.1117/12.927068
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Cited by 2 scholarly publications.
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KEYWORDS
Camera shutters

Actuators

Current controlled current source

Calibration

Cryogenics

Fourier transforms

Space telescopes

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