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Sun CubE OnE: A multi-wavelength synoptic solar micro satellite
Institution:1. Department of Physics, University of Rome Tor Vergata, Via della Ricerca Scientifica 1, Rome 00133, Italy;2. INFN, Structure of Rome Tor Vergata, Via della Ricerca Scientifica 1, Rome 00133, Italy;3. Sapienza University of Rome, School of Aerospace Engineering - ARCAlab, Via Salaria 851, 00138 Rome, Italy;4. ARGOTEC S.r.l., Via Cervino 52, 10155 Turin, Italy;5. NEXT Ingegneria dei Sistemi S.p.A., Via Giacomo Peroni 452, 00131 Roma, Italy;6. Optec S.p.A., Via Mantegna 34, 20015 Parabiago, MI, Italy
Abstract:The Sun cubE onE (SEE) is a 12U CubeSat mission proposed for a phase A/B study to the Italian Space Agency that will investigate Gamma and X-ray fluxes and ultraviolet (UV) solar emission to support studies in Sun-Earth interaction and Space Weather from LEO. More in detail, SEE’s primary goals are to measure the flares emission from soft-X to Gamma ray energy range and to monitor the solar activity in the Fraunhofer Mg II doublet at 280 nm, taking advantage of a full disk imager payload. The Gamma and X-ray fluxes will be studied with unprecedented temporal resolution and with a multi-wavelength approach thanks to the combined use of silicon photodiode and silicon photomultiplier (SiPM) -based detectors. The flare spectrum will be explored from the keV to the MeV range of energies by the same payload, and with a cadence up to 10 kHz and with single-photon detection capabilities to unveil the sources of the solar flares. The energy range covers the same bands used by GOES satellites, which are the standard bands for flare magnitude definition. At the same time SiPM detectors combined with scintillators allow to cover the non-thermal bremsstrahlung emission in the gamma energy range. Given its UV imaging capabilities, SEE will be a key space asset to support detailed studies on solar activity, especially in relation to ultraviolet radiation which strongly interacts with the upper layers of the Earth’s atmosphere, and in relation to space safety, included in the field of human space exploration. The main goal for the UV payload is to study the evolution of the solar UV emission in the Mg II band at two different time scales: yearly variations along the solar cycle and transient variations during flare events. The Mg II index is commonly used as a proxy of the solar activity in the Sun-as-a-star paradigm, in which solar irradiance variations in the UV correlate with the variations in stratospheric ozone concentrations and other physical parameters of the Earth high atmosphere. SEE data will be used together with space and ground-based observatories that provide Solar data (e.g. Solar Orbiter, IRIS, GONG, TSST), high energy particle fluxes (e.g. GOES, MAXI, CSES) and geomagnetic data in a multi-instrument/multi-wavelength/multi-messenger approach.
Keywords:Solar activity  Solar activity indices  Space weather  UV imager  X-ray  CubeSat
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