KOMPSAT-3 provides 0.7m panchromatic and 2.8m multispectral imagery. • After the separation of KOMPSAT-3 spacecraft at 16 minutes into the flight, the GCOM-W1 spacecraft separated from the launch vehicle 23 minutes after launch (Ref. The objective is to provide observation continuity from the KOMPSAT-1 and KOMPSAT-2 missions to meet the nation's needs for high-resolution optical imagery required for GIS (Geographical Information Systems) and other environmental, agricultural and oceanographic monitoring applications. Tilt, Table 4: In-orbit stability requirements of HSTS. Figure 1: Illustration of the KOMPSAT-3 spacecraft (image credit: KARI), The KOMPSAT-3 spacecraft bus design, development and integration is being led at KARI. 20 m / 100 km, Table 5: Performance parameters of the KOMPSAT missions 29), Figure 18: KOMPSAT series comparison (image credit: KARI). - Source data rate = 4 x 240 Mbit/s, Table 2: Performance parameters of the AEISS instrument. • In July 2013, ScanEx RDC of Moscow, Russia, became the official distributor of the KOMPSAT data series in Russia and the CIS countries (Ukraine, Belarus, Moldova, Kazakhstan, Uzbekistan, Kyrgyzstan, Turkmenistan, Armenia and Azerbaijan), following the signing of an agreement with the Korean company Satrec Initiative Co., Ltd. 14), • As of May 17, 2013, KOMPSAT-3 is 1 year on orbit. SESO activities did also include the mechanical design, manufacturing and mounting of the attachment flexures between the mirrors, the integration on the CFRP (Carbon Fiber Reinforced Plastics) baseplates, and the environment tests of the 5 mirrors. Figure 4: Schematic view of the payloads in the H-IIA launch vehicle (image credit: Mitsubishi) 11) 12). Figure 6: KOMPSAT-3 sample image capture of the Pentagon (image credit: Satrec Initiative, KARI), • April 8, 2013: KARI (Korea Aerospace Research Institute) has announced the start of commercial services of KOMPSAT-3 after in-orbit validation on 29 March, 2013. Image Receiving and Processing Station and several key subsystems of Mission Control Station is currently being developed. The CEUP and CC modules are actually part of the spacecraft bus, while the FPA is integrated with OM to constitute EOS. A check-up of the condition, attitude control systems, and on-board equipment has confirmed that the KOMPSAT-3 is functioning normally. 520-600 nm MS2, green PADS includes simulated sensor data generator, data analysis tools, validation tools as well as animation tools. The deployment mechanism is based on an earlier patented design by SpaceTech exhibiting very low friction, high torque margin and at the same time low deployment shock through a cam/spring driven system. The panels are rigid and can not be moved to track the sun. %20Source%20for%20test%20and%20calibration%20of%20radiometers%20_SPIE 28), 1 m (Pan) / 15 km 20), Figure 9: Comparison of an image scene observed by AEISS on KOMPSAT-3 (right) and observed by MSC on KOMPSAT-2 (left), image credit: KARI. Figure 10: Schematic view of the EOS configuration (image credit: KARI). 450-520 nm MS1 (Multispectral), blue Figure 16: Configuration of the AEISS optical system (image credit: KARI, EADS Astrium), Figure 17: Alternate view of the AEISS optical system (image credit: KARI, EADS Astrium), AEISS pre-flight calibration: A LUIS (Large Uniform Light Source) was used for the electro-optical tests of the payload such as signal to noise ratio, linearity, saturation and uniformity of radiometric response. There are two major subsystems to AEISS: EOS and the OM (Optical Module) with the telescope. The information compiled and edited in this article was provided by Herbert J. Kramer from his documentation of: ”Observation of the Earth and Its Environment: Survey of Missions and Sensors” (Springer Verlag) as well as many other sources after the publication of the 4th edition in 2002. The mission is funded by MEST (Ministry of Education, Science and Technology). 21) 22) 23) 24). This satellite agility permits event monitoring as well as single-pass stereoscopic observations. 18), Figure 7: KOMSAT-3 test image of Niagara Falls, USA, Canada (image credit: KARI, Ref. The project was started in 2004. - SI developed OBC (On-Board Processor) module with reliable RTOS and high-end CPU. - All mirrors (5) are of Zerodur design Observation of the Earth and its Environment.
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