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Ozone monitoring instrument

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1597041

Ozone monitoring instrument

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Ozone monitoring instrument

The ozone monitoring instrument (OMI) is a nadir-viewing visual and ultraviolet spectrometer aboard the NASA Aura spacecraft, which is part of the satellite constellation A-Train. In this group of satellites Aura flies in formation about 15 minutes behind Aqua satellite, both of which orbit the Earth in a polar Sun-synchronous pattern, and which provides nearly global coverage in one day. Aura satellite was launched on July 15, 2004, and OMI has collected data since August 9, 2004.

From a technical point of view, OMI instrument use hyperspectral imaging to observe solar-backscatter radiation to the space with an spectral range that covers the visible and ultraviolet. Its spectral capabilities were designed to achieve specific requirements of total ozone amounts retrievals in terms of accuracy and precision. Also its characteristics provide accurate radiometric and wavelength self calibration over the long-term project requirements.

The OMI project is a cooperation between the Netherlands Agency for Aerospace Programmes (NIVR), the Finnish Meteorological Institute (FMI) and the National Aeronautics and Space Agency (NASA).

The OMI project was carried out under the direction of the NIVR and financed by the Dutch Ministries of Economic Affairs, Transport and Public Works and the Ministry of Education and Science. The instrument was built by Dutch Space in co-operation with Netherlands Organisation for Applied Scientific Research Science and Industry and Netherlands Institute for Space Research. The Finnish industry supplied the electronics. The scientific part of the OMI project is managed by KNMI (principal investigator Prof. Dr. P. F. Levelt now at the Delft University of Technology), in close co-operation with NASA and the Finnish Meteorological Institute.

One of the scientific objectives of OMI is to measure trace gases: ozone (O3), nitrogen dioxide (NO2), sulfur dioxide (SO2), formaldehyde (HCHO), BrO, and OClO. However, OMI sensors can distinguish between aerosol types, such as smoke, dust, and sulfates, and can measure cloud pressure and cloud coverage, which provide data to derive tropospheric ozone. In that regard OMI follows in the heritage of TOMS, SBUV, GOME, SCIAMACHY, and GOMOS. On top of that, OMI aims to detect emissions in volcanic eruptions with up to at least 100 times more sensitivity than TOMS. The Ozone Monitoring Instrument has been proved an useful platform to monitor other traces gases like Glyoxal, variables like surface UV radiation, or total column estimations like the water vapor, NO2 and Ozone. Has been uses in operational services by European Centre for Medium-range Weather Forecasts (ECMWF), the US National Oceanic and Atmospheric Administration (NOAA) for ozone and air quality forecasts, and the Volcanic Ash Advisory Centers (VAACs) for the rerouting of aircraft in case of a volcanic eruption.

The instrument observes Earth's backscattered radiation and uses two imaging grating spectrometers, and each grating spectrometer is coupled to a CCD detector with 780x576 (spectral x spatial) pixels. The instrument can operate in two different modes: the normal operational mode where a single pixel in the observation has an spatial resolution 13x24 km2 at nadir (straight down), and the zoom mode where this resolution is increased to 13x12 km2.

OMI measurements cover a spectral region of 264–504 nm (nanometers) with a spectral resolution between 0.42 nm and 0.63 nm and a nominal ground footprint of 13 × 24 km2 at nadir. This spectral coverage is divided in three different channels two of them in the ultraviolet range, and one in the visible spectrum. Note that the ground pixel size of the UV-1 channel is twice as large in the swath direction compared to the other two channels, this optical design of the UV channel were done to reduce straylight in this wavelength range.

The Aura satellite orbits at an altitude of 705 km in a sun-synchronous polar orbit with an exact 16-day repeat cycle and with a local equator crossing time of 13. 45 ( 1:45 P.M.) on the ascending node. The orbital inclination is 98.1 degrees, providing latitudinal coverage from 82° N to 82° S. It is a wide-field-imaging spectrometer with a 114° across-track viewing angle range that provides a 2600 km wide swath, enabling measurements with a daily global coverage.

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