Science of SPARCS

Mission Science and Instruments

Mission Objectives

Low-mass main sequence stars of spectral type M and K are the primary stellar constituents of the Galaxy, with stellar masses ranging from about 10% to 80% of the mass of the Sun. Statistical studies based on the results of exoplanet-hunting survey missions estimate that fifty billion of these stars host at least one small planet within their habitable zone (HZ) — the narrow region around a star where temperatures allow for liquid surface water. Given their large population and the high frequency of planets orbiting them, these red dwarfs represent some of the most promising targets in the search for habitable Earth-like exoplanets.
However, the habitability of red dwarf systems is complicated by the powerful and highly variable ultraviolet (UV) radiation from the host stars. These stars are known to remain active for much of their lifetimes, maintaining elevated UV emission levels and frequent flaring for up to a billion years, particularly for the lowest-mass M stars. This radiation plays a critical role in shaping planetary atmospheres by driving atmospheric loss, altering chemical composition, and influencing overall habitability. UV photons are capable of dissociating atmospheric molecules, fundamentally changing atmospheric chemistry and potentially masking or mimicking the spectral biosignatures used to evaluate planetary habitability.
Stellar UV radiation strongly impacts key planetary atmosphere constituents such as water, ozone, sulfur dioxide (a tracer of volcanic activity), and ammonia (an essential precursor for amino acid synthesis). This impact is even stronger for planets orbiting K and M dwarfs due to their compact habitable zones, which lie just 0.1 to 0.4 AU from the host star. Furthermore, these low-mass stars exhibit far-UV (FUV) to near-UV (NUV) flux ratios that exceed the Sun's by two to three orders of magnitude. Such a spectral energy distribution leads to enhanced production of oxygen and ozone in planetary atmospheres. While this can influence habitability, it may also generate false-positive biosignatures, complicating the interpretation of exoplanet observations.
Despite the importance of UV radiation, the characteristics of UV flares on low-mass stars —specifically their occurrence rate, energy distribution, and long-term evolution — are not well constrained. UV emission does not reach the Earth's surface, such that low-mass star UV flare studies have to rely on space-based observatories. While legacy space-based missions such as the International Ultraviolet Explorer (IUE), the Galaxy Evolution Explorer (GALEX), and the Hubble Space Telescope (HST) have provided valuable insights, none were designed to systematically study the long-term UV behavior of low-mass stars. Existing observations typically consist of short exposures lasting minutes to hours. This lack of long-term continuous monitoring makes it difficult to statistically quantify rare, high-energy flares or understand long-term variability.

To address this observational gap, the Star-Planet Activity Research CubeSat (SPARCS) has been developed as the first mission dedicated to monitoring the time-dependent UV radiation of low-mass stars. SPARCS is a 6U CubeSat (30 cm × 20 cm × 10 cm) that will monitor low-mass stars in two ultraviolet bands: the near-UV (NUV; 260-300 nm, centered on the Mg II emission line in low-mass stars) and the far-UV (FUV; 153-171 nm, encompassing the C IV and He II emission lines). These wavelength ranges are highly sensitive to stellar flares and are vital for modeling the evolution of exoplanetary atmospheres and quantifying atmospheric escape rates on orbiting planets.

SPARCS is designed to probe both short- and long-term stellar UV variability, capturing everything from rapid flaring events to slow modulations of the quiescent (non-flaring) emission. The SPARCS NUV band probes chromospheric variability, while the FUV band looks into events occurring in the transition region, thus offering critical empirical data for refining stellar activity models. These models will, in turn, be used to predict exoplanet atmospheric spectra and help better interpret spectroscopic observations conducted by facilities like the James Webb Space Telescope (JWST).
During its one-year primary mission, SPARCS is expected to observe 20 low-mass stars spanning spectral types K0 to M5, including both active and inactive stars, as well as young and old systems. Target brightness ranges from approximately 1 mJy to 16 Jy at 280 nm.
SPARCS is expected to be inserted into a sun-synchronous orbit, which will enable near-continuous monitoring of each target for durations of 5 to 40 days, covering one to three full stellar rotation periods. This observing strategy allows SPARCS to measure slow rotational modulation of the quiescent stellar flux due to surface spot activity, as well as to detect and characterize stellar flares across a wide range of energies. By increasing cumulative UV exposure time by roughly three orders of magnitude compared to existing archival data, the mission will establish robust UV flare frequency distributions (FFDs) and record the rare, high-energy events that have escaped detection by previous short-duration observations.
Beyond its scientific goals, SPARCS also serves as a key technology demonstrator for next-generation ultraviolet astronomy. The SPARCS science instrument uses a UV camera (SPARCam) incorporating delta-doped CCD detectors developed at the Jet Propulsion Laboratory. These detectors provide nearly 100% internal quantum efficiency (QE) throughout the UV range and feature integrated bandpass filters optimized for FUV observations. By validating these high-performance detectors in a space environment, SPARCS will establish the technical readiness required for future flagship initiatives, most notably the Habitable Worlds Observatory.
Through its science, technology development, and educational impact, SPARCS plays a pivotal role in advancing our understanding of stellar activity, exoplanet environments, and the long-term habitability of planets orbiting low-mass stars. 

Science Instrument Payload

The SPARCS science instrument payload occupies a 3U volume (10 cm × 20 cm × 10 cm) in the spacecraft bus. It was designed to be compact and have no moving parts to mitigate cost and operational risk. It consists of a reflective telescope, a dichroic, the dualband UV camera (SPARCam), a payload processor board, and a thermal controller board. The optical system was designed to minimize the number of reflections and transmissions. The telescope is a two-mirror Ritchey-Chretien system with a 9-cm aperture. To ensure high performance in the ultraviolet, the aluminum mirrors were coated with Magnesium Fluoride (MgF₂), which prevents oxidation and maintains reflectivity above 80% across the target bands. The telescope structure was constructed with low thermal expansion (CTE) materials in order to ensure focal stability across a wide temperature range (−40ºC to 60ºC). After passing through the telescope optical system, the incoming light is divided by a dichroic beam splitter at 233 nm, which reflects the FUV signal and transmits the NUV signal to allow for simultaneous dual-band image recording at the focal plane.

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The SPARCS payload consisting of a telescope with a 9-cm primary mirror and a 3.25 cm secondary mirror feeding a dichroic beam splitter which transmits light to a NUV detector and reflects light to a FUV detector.

 

The SPARCS camera (SPARCam) adopts two high-QE, UV-optimized, backside-illuminated 1k × 1k Charge-Coupled Device (CCD) detectors from Teledyne-e2v (CCD47-20). Both detectors are 2D-doped and anti-reflection coated. The 2D-doping process applies a precise atomic layer to the sensor’s rear surface to eliminate Si/SiO₂ traps and achieve the theoretical maximum internal QE. The addition of an anti-reflection coating results in an overall QE value exceeding 30%. During science observations, the SPARCam detectors are cooled down to -35ºC to minimize noise contribution of dark current.

 

The SPARCS onboard payload processor is equipped with an autonomous dynamic detector integration time controller to both ensure adequate S/N during quiescence and allow for a proper time resolution of flaring events while mitigating the occurrence of pixel saturation. Owing to dynamic exposure control, frame integration times will vary from 1 s to 10 min. The upper end of that range was chosen to mitigate image artifacts induced by cosmic ray hits. The dynamic exposure control algorithm applies basic image processing to accurately assess integration times, but only saves raw data to disk to be further transmitted to the ground. The payload processor software extracts 2.65′ × 2.65′ regions around the targets of interest in the raw, unprocessed full-frame images (FFIs) and saves them to disk. Raw FFIs will be also saved occasionally, at a rate of ≥1 FFI per hour.

Science Targets

SPARCS can observe objects within ±40º off the ecliptic.

 

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Target List
 
The table below shows the SPARCS notional primary science target list, consisting of twenty K0 to M5 low-mass stars. Frame integration times will be between 1 s to 10 min. Objects marked with an asterisk exceed Sun avoidance constraints –  it is not guaranteed that they will be observed but their observability will be reassessed after payload commissioning. Since the SPARCS field of view is ~40′ wide, each SPARCS primary science target field will have the primary science target roughly at the center of the field, along with other secondary science/calibration targets of interest within ~20′ of the primary science target. During a science observing run, the SPARCS onboard processor extracts 2.65′ × 2.65′ subraster regions around the primary and secondary targets of interest in the raw, unprocessed full-frame images (FFIs) and saves them to disk to be transferred to the ground stations. Raw FFIs will be also saved occasionally, at a rate of ≥1 FFI per hour. If you are interested in proposing secondary targets in one of the SPARCS science target fields, complete and submit the SPARCS secondary science target subraster proposal form.

 

SPARCS Target Table
Reason to ObserveNameSpectral
Type
RADecAgeRotation
Period
SPARCS
FUV
SPARCS
NUV
Total Stare
Time
     MyrdaysµJyµJydays
YoungTW HydraeM0/K811 01 51.9053285064-34 42 17.033218380103.625581.84E+0510
Young with diskTWA 7M2V10 42 30.1018928760-33 40 16.229805204125.01921.23E+0310
YoungAO MenK406 18 28.2078302088-72 02 41.447954904222.7678.91E+0310
Young planets, disk hostAU MicM120 45 09.5324974119-31 20 27.237889841224.85103.42E+0310
YoungAF PscM4.523 31 44.9255654328-02 44 39.537845376221.12761.53E+035
Young planet, disk hostTYC 1766-1431-1M1V02 23 26.6464321080+22 44 06.759592152223.6858.83E+0218
YoungBD+20 1790K507 23 43.5893479416+20 24 58.6506458161502.71471.09E+0310
YoungHIP 106231K321 31 01.7140062576+23 20 07.3740155641500.4691.09E+055
YoungAD LeoM4V10 19 36.2808181226+19 52 12.01044657125-3002.24803.54E+035
Intermediate-age planet, disk hosteps Eri / GJ 144K203 32 55.8444911587-09 27 29.739493865200 - 80011.318201.60E+0712
Intermediate ageBZ Cet / HIP 13976K2.503 00 02.8119278075+07 44 59.1183743976259.61662.63E+056
Intermediate ageTW PsA / GJ 879K422 56 24.0525564918-31 33 56.03058476744010.31033.95E+0510
Intermediate ageHIP 20951K004 29 31.6063777896+17 53 35.4601796286259.61181.11E+0512
Intermediate ageHIP 18327K003 55 06.5013825432+16 59 54.5206716966259.8878.22E+0410
Intermediate ageHIP 23701K205 05 40.3801057412+06 27 54.72458615362510.4325.03E+0410
Intermediate age planet hostGJ 338 BM0V09 14 22.7748624830+52 41 11.7915033531000-700016.61222.89E+0317
Oldsig Dra / GJ 764K019 32 21.5902098601+69 39 40.2358052065000311801.23E+0627
Old planet hostGl 411M2V11 03 20.1948195942+35 58 11.576182057500056815.04E+0317
OldGJ 380M0/K810 11 22.1399492383+49 27 15.251007087500011.7229.15E+0412
OldGJ 825M1/M221 17 15.2690680973-38 52 02.5039385815000403513.87E+0340
SPARCS Target Table

 

 

The figure below shows the yearly visibility windows of the notional SPARCS primary science targets, taking into account Sun/Moon/Earth avoidance constraints and other spacecraft orbital constraints.

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Timeline
SPARCS

Target Proposal

Since the SPARCS field of view is ~40′ wide, each SPARCS primary science target field will have the primary science target roughly at the center of the field, along with other secondary science/calibration targets of interest within ~20′ of the primary science target. During a science observing run, the SPARCS onboard processor extracts 2.65′ × 2.65′ subraster regions around the primary and secondary targets of interest in the raw, unprocessed full-frame images (FFIs) and saves them to disk to be transferred to the ground stations. Raw FFIs will be also saved occasionally, at a rate of ≥1 FFI per hour. If you are interested in proposing secondary targets in one of the SPARCS science target fields, fill in this form. Targets brighter than NUVGALEX = 16.3 and FUVGALEX = 15.8 are expected to have a S/N ≥ 3 in a 10 min integration.