TY - JOUR
T1 - The Star-Planet Activity Research CubeSat (SPARCS)
T2 - 73rd International Astronautical Congress, IAC 2022
AU - Ardila, David R.
AU - Shkolnik, Evgenya
AU - Scowen, Paul
AU - Jacobs, Daniel
AU - Gregory, Dawn
AU - Barman, Travis
AU - Basset, Christopher
AU - Bowman, Judd
AU - Cheng, Samuel
AU - Gamaut, Jonathan
AU - Jensen, Logan
AU - Jewell, April
AU - Kolonapis, Matthew
AU - Knapp, Mary
AU - Kolopanis, Matthew
AU - Llama, Joseph
AU - Parke Loyd, R. O.
AU - Meadows, Victoria
AU - Nikzad, Shouleh
AU - Peacock, Sara
AU - Ramiaramanantsoa, Tahina
AU - Struebel, Nathaniel
AU - Swain, Mark
N1 - Funding Information: The SPARCS project acknowledges the support of the NASA via the APRA program NNH20ZDA001N- APRA. The research was carried out at the Jet Propulsion Laboratory, California Institute of Technology, operated under a contract with NASA (80NM0018D0004). Copyright 2022. California Institute of Technology. Government sponsorship acknowledged. Funding Information: The SPARCS project acknowledges the support of the NASA via the APRA program NNH20ZDA001NAPRA. The research was carried out at the Jet Propulsion Laboratory, California Institute of Technology, operated under a contract with NASA (80NM0018D0004). Copyright 2022. California Institute of Technology. Government sponsorship acknowledged. Publisher Copyright: Copyright © 2022 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2022
Y1 - 2022
N2 - Seventy-five billion low-mass stars in our galaxy host at least one small planet in their habitable zone (HZ). The stellar ultraviolet (UV) radiation received by the planets is strong and highly variable, and has consequences for atmospheric loss, composition, and habitability. These effects are amplified by the extreme proximity of the stellar HZs (0.1-0.4 AU) in low-mass stars. SPARCS is a NASA-funded mission to characterize the quiescent and flare UV emission from low-mass stars. SPARCS will observe 10 to 20 low-mass stars, over timescales of days, simultaneously in two UV bands: 153-171 nm and 260-300 nm. SPARCS Sun-synchronous terminator orbit allows for long periods of uninterrupted observations, reaching 10s of days for some targets. The payload consists of a 10 cm-class telescope, a dichroic element, UV detectors and associated electronics, a thermal control system, and an on-board processor. The payload is hosted on a Blue Canyon Technologies 6U CubeSat. SPARCS hosts several technology innovations that have broad applicability to other missions. The payload demonstrates the use of "2D-doped" (i.e., delta- and superlattice-doped) detectors and detector-integrated metal dielectric filters in space. This detector technology provides ~5x larger quantum efficiency than NASA's GALEX detectors. In addition, SPARCS' payload processor provides dynamic exposure control, automatically adjusting the exposure time to avoid flare saturation and to time-resolve the strongest stellar flares. A simple passive cooling system maintains the detector temperature under 238K to minimize dark current. The spacecraft bus provides pointing jitter smaller than 6", minimizing the impact of flat-field errors, dark current, and read-noise. All these elements enable competitive astrophysics science within a CubeSat platform. SPARCS is currently in the final design and fabrication phase (Phase C in the NASA context). It will be launched in 2024, for a primary science mission of one year.
AB - Seventy-five billion low-mass stars in our galaxy host at least one small planet in their habitable zone (HZ). The stellar ultraviolet (UV) radiation received by the planets is strong and highly variable, and has consequences for atmospheric loss, composition, and habitability. These effects are amplified by the extreme proximity of the stellar HZs (0.1-0.4 AU) in low-mass stars. SPARCS is a NASA-funded mission to characterize the quiescent and flare UV emission from low-mass stars. SPARCS will observe 10 to 20 low-mass stars, over timescales of days, simultaneously in two UV bands: 153-171 nm and 260-300 nm. SPARCS Sun-synchronous terminator orbit allows for long periods of uninterrupted observations, reaching 10s of days for some targets. The payload consists of a 10 cm-class telescope, a dichroic element, UV detectors and associated electronics, a thermal control system, and an on-board processor. The payload is hosted on a Blue Canyon Technologies 6U CubeSat. SPARCS hosts several technology innovations that have broad applicability to other missions. The payload demonstrates the use of "2D-doped" (i.e., delta- and superlattice-doped) detectors and detector-integrated metal dielectric filters in space. This detector technology provides ~5x larger quantum efficiency than NASA's GALEX detectors. In addition, SPARCS' payload processor provides dynamic exposure control, automatically adjusting the exposure time to avoid flare saturation and to time-resolve the strongest stellar flares. A simple passive cooling system maintains the detector temperature under 238K to minimize dark current. The spacecraft bus provides pointing jitter smaller than 6", minimizing the impact of flat-field errors, dark current, and read-noise. All these elements enable competitive astrophysics science within a CubeSat platform. SPARCS is currently in the final design and fabrication phase (Phase C in the NASA context). It will be launched in 2024, for a primary science mission of one year.
KW - Astrophysics
KW - CubeSats
KW - Exoplanets
KW - NASA
KW - Stars
KW - Ultraviolet
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M3 - Conference article
SN - 0074-1795
VL - 2022-September
JO - Proceedings of the International Astronautical Congress, IAC
JF - Proceedings of the International Astronautical Congress, IAC
Y2 - 18 September 2022 through 22 September 2022
ER -