A51A-3003:
GEOSTATIONARY ENVIRONMENT MONITORING SPECTROMETER (GEMS) OVER THE KOREA PENINSULA AND ASIA-PACIFIC REGION

Friday, 19 December 2014
James Lasnik1, Michelle Stephens1, Brian Baker1, Christopher Randall1, Dai Ho Ko2, Seonghui Kim2, Youngsun Kim2, Eung Shik Lee2, Suyoung Chang2, Jong-Moon Park2, Seok-Bae SEO2, Youngchun Youk2, Jong Pil Kong2, Deoggyu Lee2, Seung-Hoon Lee2 and Jhoon Kim3, (1)Ball Aerospace & Technologies, Boulder, CO, United States, (2)Korea Aerospace Research Institute, Daejeon, South Korea, (3)Yonsei University, Seoul, South Korea
Abstract:
Introduction: The Geostationary Environment Monitoring Spectrometer (GEMS) is one of two instruments manifested aboard the South Korean Geostationary Earth Orbit KOrea Multi-Purpose SATellite-2B (GEO-KOMPSAT-2B or GK2B), which is scheduled to launch in 2018. Jointly developed/built by KARI and Ball Aerospace, GEMS is a geostationary UV-Vis hyperspectral imager designed to monitor trans-boundary tropospheric pollution events over the Korean peninsula and Asia-Pacific region. The spectrometer provides high temporal and spatial resolution (3.5 km N/S by 7.2 km E/W) measurements of ozone, its precursors, and aerosols. Over the short-term, hourly measurements by GEMS will improve early warnings for potentially dangerous pollution events and monitor population exposure. Over the 10-year mission-life, GEMS will serve to enhance our understanding of long-term climate change and broader air quality issues on both a regional and global scale. The GEMS sensor design and performance are discussed, which includes an overview of measurement capabilities and the on-orbit concept of operations.

GEMS Sensor Overview: The GEMS hyperspectral imaging system consists of a telescope and Offner grating spectrometer that feeds a single CCD detector array. A spectral range of 300-500 nm and sampling of 0.2 nm enables NO2, SO2, HCHO, O3, and aerosol retrieval. The GEMS field of regard (FOR), which extends from 5°S to 45°N in latitude and 75°E to 145°E in longitude, is operationally achieved using an onboard two-axis scan mirror. On-orbit, the radiometric calibration is maintained using solar measurements, which are performed using two onboard diffusers: a working diffuser that is deployed routinely for the purpose of solar calibration, and a reference diffuser that is deployed sparingly for the purpose of monitoring working diffuser performance degradation.