Learn about the ground-based, ship-borne, balloon-borne, and airborne campaigns and small satellite field experiments that validate orbiting ESA EO satellites and support future mission development.
The current mission design envisages flying two separate radars on separate platforms.
objectives were: Improving the parameterizations of the dependencies between sea surface emissivity at L-band and surface roughness, and perform validation of currently
However, the phases seem to be anti-correlated, which is currently being investigated.
The CReSIS radar is a classic nadir-looking altimeter, i.e. the current system configuration does not support acquisition in the SAR nor SARIn mode that