GLO: A SOLAR OCCULTATION INSTRUMENT SUITABLE FOR CONSTELLATIONS OF SMALL SATELLITES A KEY CHALLENGE IN THE EARTH SCIENCE COMMUNITY IS TO EXPLOIT RAPIDLY ADVANCING MICROSATELLITE (MICROSAT) TECHNOLOGY IN THE TASK OF PROVIDING THE MYRIAD OF GLOBAL MEASUREMENTS REQUIRED TO UNDERSTAND KEY PROCESSES. MICROSATS OFFER THE POSSIBILITY OF INEXPENSIVE ACCESS TO SPACE BUT ALSO PRESENT PAYLOAD DESIGN CHALLENGES RESULTING FROM ISSUES SUCH AS LIMITED SIZE WEIGHT AND POWER (SWAP) CAPACITY AND POINTING CAPABILITY. WE PROPOSE A TECHNOLOGY DEMONSTRATION OF AN INSTRUMENT WE REFER TO AS GLO (GFCR (GAS FILTER CORRELATION RADIOMETRY) LIMB SOLAR OCCULTATION) WHICH WOULD MEASURE THE VERTICAL PROFILE OF ATMOSPHERIC TRACE SPECIES WITH STATE-OF-THE-ART ACCURACY. GLO CONTAINS 23 VISIBLE NEAR INFRARED (VNIR) AND SHORT WAVELENGTH INFRARED (SWIR) SPECTRAL BANDS AND MEASURES 10 CONSTITUENTS PLUS TEMPERATURE (T) YET FITS INTO A 29X16X16 CM FORM FACTOR WEIGHS 5.25 KG CONSUMES JUST 28.2 W DURING OBSERVATIONS AND DOES NOT LEVY STRINGENT POINTING REQUIREMENTS TO THE SPACECRAFT. GLO HAS HERITAGE FROM HALOE AND AIM/ SOFIE BOTH HIGHLY SUCCESSFUL SOLAR OCCULTATION (SO) INSTRUMENTS BUT (USING RECENT ADVANCES IN FOCAL PLANE ARRAY (FPA) AND COOLER TECHNOLOGY) IS MUCH SMALLER AND REQUIRES SUBSTANTIALLY LESS POWER. IN ADDITION IT HAS SIGNIFICANTLY IMPROVED VERTICAL RESOLUTION POINTING AND UPPER TROPOSPHERE AND LOWER STRATOSPHERE (UTLS) AEROSOL AND T MEASUREMENT CAPABILITY AS WELL AS MUCH REDUCED SENSITIVITY TO AEROSOL CONTAMINATION IN TRACE GAS RETRIEVALS. NOVEL ASPECTS OF THE GLO SENSOR INCLUDE: USE OF TACTICAL BUT SPACE QUALIFIED IMAGING FPAS (LOW COST); GFCR WITH IMAGING ARRAYS (PRECISE CHANNEL COALIGNMENT AND REGISTRATION); PROXY GFCR FOR UTLS H2O AND O3 (INCREASED INSENSITIVITY TO AEROSOL CONTAMINATION IN THE UTLS); AND VNR PLUS SWIR AEROSOL EXTINCTION MEASUREMENT CAPABILITY (AEROSOL EXTINCTION PLUS BULK PROPERTIES). WHILE GLO COULD HAVE MANY APPLICATIONS (INCLUDING E.G. AN INEXPENSIVE STRATOSPHERIC MONITORING SENSOR) WE CONCEIVED IT TO PROBE A KEY BUT POORLY DOCUMENTED COMPONENT OF THE CLIMATE SYSTEM THE UTLS IN A MISSION CONCEPT REFERRED TO AS SOCRATES (SOLAR OCCULTATION CONSTELLATION FOR RETRIEVING AEROSOLS AND TRACE ELEMENT SPECIES). THE GOAL OF SOCRATES IS TO QUANTIFY THE ROLE OF THE UTLS IN CLIMATE CHANGE. FOR SOCRATES GLO MEASURES T RADIATIVELY ACTIVE GASES (H2O O3 CH4 N2O) AEROSOLS AND TRANSPORT TRACERS (HDO CO HCN HF HCL) WITH VERTICAL RESOLUTION (<1 KM) AND GEOGRAPHIC SAMPLING REQUIRED FOR UTLS RADIATIVE FORCING CALCULATIONS. SATELLITE SO INSTRUMENTS PROVIDE HIGH VERTICAL RESOLUTION AND PRECISION BUT SAMPLE ONLY 2 LATITUDES PER ORBIT. TO MITIGATE THIS SHORTCOMING SOCRATES CONSISTS OF A CONSTELLATION OF 6 GLO SENSORS DEPLOYED FROM A SINGLE LAUNCH VEHICLE INTO ORBITS WITH SLIGHTLY DIFFERENT MEAN ALTITUDES. THE DISPERSING ORBITS PROVIDE THE REQUIRED SPATIAL AND TEMPORAL SAMPLING WITH COVERAGE FROM 65 LATITUDE. WE HAVE SHOWN THAT THE SOCRATES GLO CONSTELLATION (6 SENSORS AND MICROSATS) MEETS ALL MEASUREMENT COMPLEMENT ACCURACY VERTICAL RESOLUTION AND SPATIAL SAMPLING REQUIREMENTS AND CAN BE FABRICATED LAUNCHED AND OPERATED IN A 26-MONTH MISSION WITHIN THE NASA EARTH VENTURE MISSION COST CAPPED BUDGET.UNDER THIS PROPOSAL WE WILL REFINE THE DESIGN AND FABRICATE A COMPLETE PROTOTYPE GLO SENSOR [IDENTICAL IN FORM FIT AND FUNCTION TO THE SOCRATES/GLO SENSOR EXCEPT FOR THE USE OF NON-SPACE QUALIFIED (BUT FUNCTIONALLY IDENTICAL) COMPONENTS] PERFORM FUNCTIONAL AND ENVIRONMENTAL TESTS TO CONFIRM IT CAN MEET SOCRATES MEASUREMENT REQUIREMENTS AND VALIDATE THE INSTRUMENT CONCEPT THROUGH GROUND AND BALLOON-BASED OBSERVATIONS. THIS WILL PROVIDE A NEARLY COMPLETE DEMONSTRATION OF THE GLO TECHNOLOGY AND MEASUREMENT APPROACH AND CAPABILITIES. THE GOAL IS TO RAISE THE GLO SENSOR TECHNIQUE AND DESIGN FROM TRL 4 TO TRL 6 PROVIDING RISK REDUCTION FOR THE SOCRATES MISSION CONCEPT AND FOR THE USE OF GLO IN OTHER MISSIONS.