Here we describe two new systems recently funded by the NASA Earth Science Technology Office (ESTO) to improve present capabilities for high-resolution atmospheric sensing from small satellite platforms. First, the Configurable Reflectarray Wideband Scanning Radiometer (CREWSR) is a high-resolution, lightweight, low-power multiband (23, 31, and 50-58 GHz) radiometer with a deployable scanning reflectarray. It is envisioned to be fielded on an ESPA-class small satellite platform, with a stowed volume that fits within a 0.61 m x 0.71 m x 0.97 m envelope. Once in orbit, the platform will deploy a large Reconfigurable Reflective Surface (RRS), as well as a multi-feed antenna connected to a multiband radiometer. These components allow for an electronically-scanned beam for radiometric Earth observation. CREWSR would operate with a single, linear polarization, but fully polarimetric operation is also possible in principle. The reflectarray is also compatible with radar use, thus enabling wide-swath radar from a small satellite.
Second, there is a critical need to enable development, test, and evaluation of Versatile, Intelligent, and Dynamic Earth Observation (VIDEO), and one key enabler is the recent emergence of metamaterials for use in high-performance blackbody radiometric targets. These materials are very thin (~200 microns) and lightweight (tens of grams), allowing them to be easily scaled up to realize very large targets (> 1 m^2) to subtend an entire sensor field of regard during laboratory measurements. Furthermore, the thin planar structure of the metamaterials provides a relatively small thermal mass, thereby permitting the projection of thermal features with very high spatial frequency content into the sensor field of view at the subpixel level. We will produce a 50 cm x 75 cm (20” x 30”) Radiometric Scene Generator (RSG) operating near 54 GHz with very large thermal contrast at the subpixel level for a typical spaceborne microwave radiometer full-width-at-half-maximum (FWHM) beam width in the range of 1-3 degrees. The RSG will be used for two purposes: (1) to project spatial features into the radiometer field of regard that can be detected and acted upon by the intelligent processing algorithms, and (2) to spatially encode spectral information in the atmospheric sounding band used for temperature profiling. The intelligent processing algorithm will utilize feature detection and machine learning techniques to recognize regions of interest in the atmospheric scene and cause the sensor to react to the scene characteristics by changing the sensor response function. In this presentation, we will provide an overview of these new technologies and discuss how they address current unmet needs for high-resolution sensing from small satellites in the critical frequency bands spanning 20-60 GHz.

