21 May 2013 Jim Leitch, PI jleitch@ball.com 303-939-5280 Geostationary Trace Gas and Aerosol Sensor Optimization (GeoTASO) ESTO IIP 21 May 2013 Jim Leitch,

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21 May 2013 Jim Leitch, PI jleitch@ball.com 303-939-5280 Geostationary Trace Gas and Aerosol Sensor Optimization (GeoTASO) ESTO IIP 21 May 2013 Jim Leitch, PI jleitch@ball.com 303-939-5280

Outline and Team NASA ESTO quad chart Ball Sensor Team: Sensor overview Project objectives Sensor status Expected sensor performance Algorithm preparation Plans Ball Sensor Team: Tom Delker, Lead Bill Good, Airborne Lead Many supporting engineers and technicians Co-Investigators Kelly Chance, Xiong Liu – Harvard/SAO Scott Janz, Ken Pickering, Nick Krotkov – NASA/GSFC Jun Wang – U Nebraska

Ball Aerospace & Technologies Corp. Proprietary Information

Sensor Concept Overview Nadir-viewing wide-swath imaging spectrometer Two channel spectrometer uses: 1st order diffraction for Visible 2nd order diffraction for UV Low polarization sensitivity telescope (<3%) and electronic depolarizer for spectrometer Field-swappable spectrometer slits to change spectral passband and sampling Selectable view: wide nadir swath or zenith look with an optical fiber Parameter Value Ground spot 40 m x 80 m Ground sample 10 m x 50 m Swath 10 km

GeoTASO Advances Mission Readiness of GEO-CAPE UV-Vis Sensing Hardware demonstration: Compact spectrometer Minimal blur depolarizer in a spectrometer Filtering scheme effectiveness Sensor-algorithm system demonstration: Real scene data with variable spectral/spatial sampling and varying polarization sensitivity Effect on algorithm of spectral dispersion/filtering in spectrometer Prediction/Validation: Component and system performance measurements inform TEMPO DISCOVER AQ contribution as “satellite analog” measurement from moderately high altitude overflights of DISCOVER-AQ test sites Flights with DISCOVER-AQ provide rich data set of measurements for comparison and validation of retrievals

Sensor Status (1 of 2) Telescope in alignment Spectrometer aligned: Built on separate baseplate Spectrometer aligned: All optics in place Initial imaging measurements made Vertical alignment (flight configuration) verified Detector alignment underway Grating ghost is < 1e-4 of signal

Sensor Status (2 of 2) Lineshape asymmetry of <4% Imaging performance predicts lineshape within specification GeoTASO sensor in its thermally-stabilized enclosure and mounting frame for the Falcon GeoTASO sensor in the nadir well with electronics racks Lineshape asymmetry of <4% Lineshape from imaging spot convolved with slit width to give passband shape Completed preliminary engineering and airworthiness reviews with Langley flight team

GeoTASO Predicted SNR SNR predictions for 1 km square ground sample Required SNRs shown as a band-averaged value (red lines) Single sample SNRs are ~100x smaller (GSD: 40 m x 80 m) NO2 NO2 SO2 CHOCHO SO2 HCHO CHOCHO O3 O3 HCHO O3 O3 3 samples/FWHM, SN03 grating, updated well and noise values, 0.6 mm flattening filter thickness

GeoTASO Predicted Saturation Attenuation of visible channel from color filter glass in telescope Adjustable amount of filtering using different filter thicknesses Shorter integration times (in snapshot mode) can capture high signal scenes for cloud/aerosol studies in O2 B band 3 samples/FWHM, SN03 grating, updated well values, 0.6 mm filter thickness, 240 ms integration time

Algorithm Work Aerosols (Jun Wang): Development of a radiative transfer model (RTM) that includes modeling of trace gases, Rayleigh scattering, Aerosol Mie scattering, radiative transfer, etc. Tests of aerosol retrieval algorithms using AERONET ground data measuring direct and diffuse solar radiance Trace Gases (Kelly Chance, Xiong Liu): Much preparation work for GeoTASO done using ACAM data from DISCOVER-AQ Sensor Effects in data Fits of slit function and spectral shifts SNR characterization Empirical sensor radiometric calibration Retrieval Studies: Derivation of reference spectrum to use in retrievals Finding best spectral fit windows Investigating direct retrievals of ozone profiles and trace gases

Plans Sensor functional testing in late June Sensor test flights at Langley in July Calibration at Goddard (common cal to ACAM) after test flights Data collection flights in September in conjunction with DISCOVER-AQ in Houston Validation of retrieval performance using comparison with other DISCOVER-AQ measurements (ground-based and airborne) B200 w/ACAM: 26 kft, 140 m/s HU-25C w/GeoT: 40 kft, 230 m/s Example of ACAM-based NO2 retrieval compared with Pandora