Colorado Ultraviolet Transit Experiment: a dedicated CubeSat mission to study exoplanetary mass loss and magnetic fields
Author
Fleming, Brian T.France, Kevin
Nell, Nicholas
Kohnert, Richard
Pool, Kelsey
Egan, Arika
Fossati, Luca
Koskinen, Tommi
Vidotto, Aline A.
Hoadley, Keri
Desert, Jean-Michel
Beasley, Matthew
Petit, Pascal M.
Affiliation
University of Arizona, Lunar and Planetary Laboratory, Tuscon, Arizona, United StatesIssue Date
2018-01
Metadata
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Brian T. Fleming, Kevin C. France, Nicholas Nell, Richard A. Kohnert, Kelsey Pool, Arika Egan, Luca Fossati, Tommi T. Koskinen, Aline A. Vidotto, Keri Hoadley, Jean-Michel Desert, Matthew Beasley, Pascal M. Petit, "Colorado Ultraviolet Transit Experiment: a dedicated CubeSat mission to study exoplanetary mass loss and magnetic fields," J. Astron. Telesc. Instrum. Syst. 4(1) 014004 (6 February 2018)Rights
© 2018 SPIE.Collection Information
This item from the UA Faculty Publications collection is made available by the University of Arizona with support from the University of Arizona Libraries. If you have questions, please contact us at repository@u.library.arizona.edu.Abstract
The Colorado Ultraviolet Transit Experiment (CUTE) is a near-UV (2550 to 3300 angstrom) 6U CubeSat mission designed to monitor transiting hot Jupiters to quantify their atmospheric mass loss and magnetic fields. CUTE will probe both atomic (Mg and Fe) and molecular (OH) lines for evidence of enhanced transit absorption, and to search for evidence of early ingress due to bow shocks ahead of the planet's orbital motion. As a dedicated mission, CUTE will observe greater than or similar to 100 spectroscopic transits of hot Jupiters over a nominal 7-month mission. This represents the equivalent of >700 orbits of the only other instrument capable of these measurements, the Hubble Space Telescope. CUTE efficiently utilizes the available CubeSat volume by means of an innovative optical design to achieve a projected effective area of similar to 28 cm(2), low instrumental background, and a spectral resolving power of R similar to 3000 over the primary science bandpass. These performance characteristics enable CUTE to discern transit depths between 0.1% and 1% in individual spectral absorption lines. We present the CUTE optical and mechanical design, a summary of the science motivation and expected results, and an overview of the projected fabrication, calibration, and launch timeline. (c) 2018 Society of Photo-Optical Instrumentation Engineers (SPIE)Note
No embargo.ISSN
2329-4124Version
Final published versionSponsors
National Aeronautics and Space Administration (NASA) [NNX17AI84G]ae974a485f413a2113503eed53cd6c53
10.1117/1.JATIS.4.1.014004