Digital Store and Forward Communication Experiment (DSFCE) CCD Earth Imaging System (CEIS) Digital Signal Processing Experiment (DSPE) Cosmic Ray Experiment (CRE)
KITSAT-1 or KITSAT-A (Korean Institute of Technology Satellite)[2] is the first South Koreansatellite to be launched. Once launched, the satellite was given the nickname "Our Star" (우리별). KITSAT-1 operated in a 818 miles (1,316 km) by 825 miles (1,328 km) low Earth orbit (LEO). Of the 12 satellites launched by South Korea, KITSAT-1 is in the highest orbit.[3] While KITSAT-1 maintains equilibrium by gravity gradient forces, magnetic torque can be used to control attitude if needed.[4] The forecasted lifespan of KITSAT-1 was only five years, but communication with the satellite was maintained for 12 years.[3] Since the launch of KITSAT-1, South Korea launched an additional 36 satellites by 2020.[2]
KITSAT-1's on-board computer (OBC) system uses an OBC186 for the main OBC and an OBC80 as the backup on-board computer system.[5]
KITSAT-1 carried a Digital Store and Forward Communication Experiment (DSFCE), a CCD Earth Imaging System (CEIS), a Digital Signal Processing Experiment (DSPE), and a Cosmic Ray Experiment (CRE).[6]
The CCD Earth Imaging System is equipped with two different cameras. These cameras are a wide-angle camera with a 4 km/pixel resolution and a high-resolution camera with a 400 m/pixel resolution.[4] The two CCD cameras on KITSAT-1 are located on the bottom of the satellite so that the cameras should always be pointed toward Earth[7]
On board was equipment to run the Cosmic Ray Experiment (CRE). The experiment's main purpose was to monitor and study space radiation in a 1,320 km (820 mi) low Earth orbit. These space radiation measurements were to be taken in short and long time frames. The CRE is able to measure high-energy protons, galactic cosmic rays from deep space, and solar cosmic rays from solar flares.[4]
The CRE payload consists of two subsystems. The two subsystems are the Cosmic Particle Experiment (CPE) and the Total Dose Experiment (TDE). The CPE is used to measure the Linear Energy Transfer (LET) spectrum over short time frames, and the TDE is used to measure the total accumulated ionizing radiation dose over long time frames.[4]
Launch
Launched in 1992, KITSAT-1, which stands for the Korea Institute of Technology Satellite-1, was the first satellite developed by SaTReC. Developed through a collaborative program between SaTReC and the University of Surrey, United Kingdom, the main objective of the KITSAT-1 program was to acquire satellite technology through the training and education of satellite engineers.[8]
^ abKim, H.S.; Lee, H.K.; Choi, S.D. (May 1996). "On-board computer system for kitsat-1 and 2"(PDF). Journal of Astronomy and Space Sciences. 13 (2): 41–51. Archived(PDF) from the original on 4 May 2021. Retrieved 29 April 2021.
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).