kompsat 3 aeiss

The IRPE provides the capability to receive and store KOMPSAT-3 data, support to collection planning, generate standard and value added imagery products, and distribute imagery products to users. Tilt, Table 4: In-orbit stability requirements of HSTS. This applies to imagery of the KOMPSAT-2, -3 and -5 missions. 10), • SDS-4 (Small Demonstration Satellite-4) of JAXA with a mass of ~ 48 kg. The development, manufacturing and testing under various load conditions (including thermal cycling) of the HSTS (High Stability Telescope Structure) was done and verified by EADS Astrium. 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. Figure 12: Photo of the FPA (view from the sensor/baffle side), image credit: DLR 25), 450-900 nm Pan (Panchromatic) • On June 15, 2012, KARI released the first image obtained by KOMPSAT-3 (Figure 9). The X-band is used to downlink the payload data. - Source data rate = 4 x 240 Mbit/s, Table 2: Performance parameters of the AEISS instrument. The spacecraft is 3-axis stabilized. KOMPSAT-3 - CSCDA (Copernicus Space Component Data Access) KOMPSAT-3 KOMPSAT-3 is a Korean remote sensing satellite, which provides 0.7 m GSD panchromatic image and 2.8 m GSD multi-spectral image data for various applications including visual … • 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. The panels are rigid and can not be moved to track the sun.

The primary payload on this flight was GCOM-W1 (Global Change Observation Mission - Water 1) of JAXA (nickname: Shizuku) with a launch mass of ~ 1990 kg. The focusing control is performed using the displacement of the heater ring attached on the upper and lower side of the telescope by heating one of two rings, thereby expecting downward or upward movement of the corresponding secondary mirror. 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. 3 m /30 km This represents the first satellite launch services order placed to MHI by an overseas customer.

The MCE provides the S-band command and telemetry communications interface to the satellite and the necessary functions to operate the satellite. Legend to Figure 9: The image scene is of Jeodong Port on Ulleungdo Island, Korea.

• The KOMPSAT-3 spacecraft and its payload are operating nominally in 2014. The First Year Anniversary For KOMPSAT-3 Is Also A Pricing Benefit (Imagery),” Satnews Daily, May 17, 2013, URL: http://www.satnews.com/story.php?number=1233155485#, 17) “Commercial sales of KOMPSAT-3 has started,” Satrec Initiative, April 8, 2013, URL: https://www.satreci.com/eng/ds1_1.html?tno=100&db=pr_board&no=25, 18) Bang-Yeop Kim, “The practical uses and application status of satellite image in Korea,” Proceedings of the 50th Session of Scientific & Technical Subcommittee of UN-COPUOS, Vienna, Austria, Feb. 11-22, 2013, URL: http://www.oosa.unvienna.org/pdf/pres/stsc2013/tech-15E.pdf, 19) “Satrec Initiative Announces Agreement with Korea Aerospace Research Institute,” Satrec Initiative, Nov. 15, 2012, URL: https://www.satreci.com/eng/ds1_1.html?tno=100&db=pr_board&no=22, 20) http://m.kari.re.kr/kor/html/news/news_view.html?num=1518¤tPage=1&searchType=&searchString=, 21) Andreas Eckardt, Anko Börner, Stefan Hilbert, Ingo Walter, “High resolution Instruments for Air-and Spaceborne Application,” DLR, DIN-WS, Nov. 20, 2006, URL: http://www2.informatik.hu-berlin.de/cv/documents/Fusion_Workshop_11.2006/02_Eckardt.pdf, 22) Jong-Pil Kong, Andreas Eckardt, Bo-Gwan Kim, “The Design of the Focal Plane Assembly for AEISS,” Proceedings of the 60th IAC (International Astronautical Congress), Daejeon, Korea, Oct. 12-16, 2009, IAC-09.B1.I.6, 23) “KOMPSAT-3 Image Data Manual,” KARI, Satrec Initiative, V1.0/ 2013.04.01, URL: http://www.geosoluciones.cl/documentos/Kompsat/KOMPSAT3_Image_Data_Manual_v1.0.pdf, 24) KOMPSAT-3 Submeter in the afternoon,” SI, URL: http://kompsat.satreci.com/ds2_3_1.html, 25) http://www.dlr.de/os/en/desktopdefault.aspx/tabid-7311/12268_read-29159/, 26) Deog-Gyu Lee, Eung-Shik Lee, Su-Young Chang, Andreas Kasemann, Dietmar Scheulen, Tom Butters, “The development of a dimensionally stable CFRP camera structure,” Proceedings of the 60th IAC (International Astronautical Congress), Daejeon, Korea, Oct. 12-16, 2009, IAC-09.C2.2.1, 27) Hélène Ducollet, Christian du Jeu, Seung-Hoon Lee, “Manufacturing of the Spaceborne Camera Mirrors for KARI's LEO Satellite,” ICSO 2010 (International Conference on Space Optics), Rhodes Island, Greece, Oct. 4-8, 2010, 28) Vikrant Mahajan, Dae-Jun Jung,, “Design and Characterization of Uniform Spectral Radiance source for test and calibration of radiometers used for KOPMSAT-3,” SPIE Proceedings Volume 6958, 'Sensors and Systems for Space Applications II,' Editors: Richard T. Howard, Pejmun Motaghedi, May 2008, URL: http://www.labsphere.com/.../Characterization%20of%20Uniform%20Spectral%20Radiance 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. Satrec Initiative will deliver high quality image data to worldwide customers through collaboration with existing satellite operators, and in addition to that, building its own KOMPSAT data distribution network. 18), Figure 7: KOMSAT-3 test image of Niagara Falls, USA, Canada (image credit: KARI, Ref. 17), • In January 2013, KOMPSAT-3 is still in the commissioning phase and should be operational soon. - Focal length = 8.6 m Figure 5: KOMPSAT-3 image of Rio de Janeiro Brazil with the Maracanã stadium acquired on April 16, 2013 and released on Jan. 03, 2014 (image credit: Satrec Initiative, KARI) 13). 1) 2) 3), SI (Satrec Initiative) of Daejeon participation in the KOMPSAT-3 development of KARI: 4) 5).
Figure 13: Logical block diagram of the CEU architecture (image credit: DLR, KARI). 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. 760-900 nm MS4, NIR (Near Infrared), - Korsch-type telescope design on a CFRP optical bench The agile spacecraft features a body pointing capability of ±45º into any direction (cross-track or along-track). - Pixel pitch = 2 x 17.5 µm - 80 cm diameter of primary mirror aperture (the mirror is lightweighted)

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