In-orbit validation of the fmpl-2 instrument—the gnss-r and l-band microwave radiometer payload of the fsscat mission

• Published in: Remote Sensing
• Main Authors: Muñoz-Martín, Joan Francesc, Fernández, Lara P., Perez, Adrian, Ruíz-de-Azúa, Joan Adrià, Park, Hyuk, Camps, Adriano, Carnicero Domínguez, Bernardo, Pastena, Massimiliano
• Other Authors: Ministerio de Economía y Competitividad (España), Generalitat de Catalunya
• Format: Article in Journal/Newspaper
• Language: unknown
• Published: Multidisciplinary Digital Publishing Institute 2020
• Subjects: GNSS-R; Microwave radiometry; L-band; CubeSat; Sea ice; Soil moisture
• Online Access: http://hdl.handle.net/10261/249615; https://doi.org/10.3390/rs13010121; https://doi.org/10.13039/501100002809; https://doi.org/10.13039/501100003329

The Flexible Microwave Payload-2 is the GNSS-R and L-band Microwave Radiometer Payload on board Cat-5/A, one of the two 6-unit CubeSats of the FSSCat mission, which were successfully launched on 3 September 2020 on Vega flight VV16. The instrument occupies nearly a single unit of the CubeSat, and its goal is to provide sea-ice extension and thickness over the poles, and soil moisture maps at low-moderate resolution over land, which will be downscaled using data from Cosine Hyperscout-2 on board Cat-5/B. The spacecrafts are in a 97.5 inclination Sun-synchronous orbit, and both the reflectometer and the radiometer have been successfully executed and validated over both the North and the South poles. This manuscript presents the results and validation of the first data sets collected by the instrument during the first two months of the mission. The results of the validation are showing a radiometric accuracy better than 2 K, and a sensitivity lower than the Kelvin. For the reflectometer, the results are showing that the sea-ice transition can be estimated even at short integration times (40 ms). The presented results shows the potential for Earth Observation missions based on CubeSats, which temporal and spatial resolution can be further increased by means of CubeSat constellations. This work was supported by 2017 ESA S3 challenge and Copernicus Masters overall winner award (“FSSCat” project). this work has been (partially) sponsored by project SPOT: Sensing with Pioneering Opportunistic Techniques grant RTI2018-099008-B-C21/AEI/10.13039/501100011033, and by the Unidad de Excelencia Maria de Maeztu MDM-2016-0600, and by the ICREA Academia award by the Generalitat de Catalunya, and by the grant for recruitment of early-stage research staff FI-DGR 2018 of the AGAUR—Generalitat de Catalunya (FEDER), Spain.