CLOUDS REMAIN AS A MAJOR SOURCE OF UNCERTAINTY IN CLIMATE MODELS. ICE CLOUDS IN PARTICULAR ARE POORLY CONSTRAINED AND HAVE BEEN USED AS A TUNING PARAMETER IN THE MODELS TO BALANCE RADIATION BUDGET AT THE TOP OF ATMOSPHERE AND PRECIPITATION AT THE SURFACE. LACK OF ACCURATE CLOUD ICE AND ITS MICROPHYSICAL PROPERTY MEASUREMENTS HAS LED TO LARGE UNCERTAINTY ABOUT GLOBAL CLOUDS AND THEIR PROCESSES WITHIN THE ATMOSPHERE. NASAS AEROSOL CLOUD AND ECOSYSTEMS ACE AN EARTH SCIENCE DECADAL SURVEY DS MISSION RECOMMENDED AN ADVANCED SCIENCE PAYLOAD WITH SUBMMWAVE AND LONGWAVE INFRARED LWIR RADIOMETERS FOR SUCH CLOUD ICE MEASUREMENT. IN A RECENT COMMUNITY WHITE PAPER CLOUD AND PRECIPITATION PROCESS MEASUREMENTS CAPPM DYNAMICS AND MICROPHYSICAL PROPERTIES ARE IDENTIFIED AS THE KEY LINKS BETWEEN THE CLOUD PRECIPITATION PROCESSES AND NEED MORE ACCURATE MEASUREMENTS. IN THIS PROJECT WE WILL DEVELOP A COMPACT SUBMM WAVE AND LWIR POLARIMETERS SWIRP INSTRUMENT TO ENABLE ACCURATE MEASUREMENTS OF CLOUD ICE AND ITS MICROPHYSICAL PROPERTIES PARTICLE SIZE AND SHAPE. RADIOMETRIC AND POLARIMETRIC MEASUREMENTS FROM THE PROPOSED SUBMM 220 AND 680 GHZ AND IR 8.6 11 AND 12 M BANDS PROVIDING THE NEEDED SENSITIVITY OVER A FULL DYNAMIC RANGE OF CLOUD ICE WILL BE USED JOINTLY IN CLOUD RETRIEVALS. THE CONICAL SCANNING CONFIGURATION WITH SWIRP WILL PRESERVE HORIZONTAL H AND VERTICAL V POLARIZATION INFORMATION FOR BULK CLOUD PARTICLE SHAPE RETRIEVALS WHILE THE SWIRPS MATCHED SUBMM AND LWIR FOOTPRINTS WILL ALLOW THE JOINT RETRIEVAL OF CLOUD PARTICLE SIZE WITH THESE FREQUENCY BANDS. THE COMPACTNESS OF SWIRP DESIGN ENABLES COST EFFECTIVE DEPLOYMENT OF THESE RADIOMETERS POLARIMETERS ON FUTURE LARGE SPACE FLIGHT MISSIONS ACE OR ON SMALL DISTRIBUTED FLIGHT SYSTEMS FOR RAPID UPDATE AND FREQUENT REVISIT SAMPLING TO STUDY FAST ATMOSPHERIC PROCESSES.IN IIP16 WE WILL SUBSTANTIATE THE TECHNICAL FEASIBILITY OF MINIATURIZING MMSUBMM POLARIMETRIC DIRECT DETECTION RECEIVERS A NOVEL MULTI CHANNEL LWIR SPECTRO POLARIMETERS AND A COMPACT BEARING AND POWER TRANSFER ASSEMBLY BAPTA FOR CONICAL SCANNING OBSERVATIONS. WE WILL BUILD A PROTOTYPE INSTRUMENT WITH SELF CALIBRATION IN A VOLUME OF 20 20 40 CM AND COMPLETE LABORATORY ENVIRONMENTAL AND ROOFTOP TESTS AT THE END OF PROJECT. THE ENTRY LEVEL FOR THE PROPOSED INSTRUMENT IS TRL 3 AND IT WILL REACH TRL S WITHIN THE 3 YEAR PERIOD OF PERFORMANCE.
$627,107FY2017National Aeronautics and Space AdministrationNASA
University Of Arizona, Tucson AZ