Satellite

01

Securing satellite development technology to meet national public demand

The research and development of satellites in Korea began in 1994 when the General Science and Technology Council approved a multipurpose satellite (Arirang) development project. The multipurpose Arirang 1 was developed in 1999 to meet public demand for satellite images, with Arirang 2 developed under the initiative in Korea in 2006. Later, Arirang 3, Arirang 5, and Arirang 3A were developed in 2012, 2013, and 2015, respectively. Currently, KARI is developing Arirang 6, a high-precision radar satellite, and Arirang 7 and Arirang 7A as cutting-edge precision earth observation optical satellites.

Moreover, it developed Cheollian 1, Korea’s first geostationary orbit satellite capable of independent meteorological and ocean observation services. It also developed—and is currently operating—Cheollian 2A, which is capable of more precise meteorological observation than Cheollian 1, and Cheollian 2B, which is capable of marine observation as well as the world’s first atmospheric environmental observation from the geostationary orbit. In particular, Cheollian 2B is expected to help resolve conflicts between countries and social problems due to fine dust by identifying the migration path of air pollutants, such as fine dust, around the Korean Peninsula.
KARI has also developed small and scientific experimental satellites, such as Science and Technology 1 in 2003 and Naro Science and Science and Technology 3 in 2013. KARI has secured its independent satellite development technology by developing multipurpose satellites and geostationary orbit satellites. 500kg next-generation mid-size satellites 1 was launched in 2021 to transfer satellite technology to private industry with the aim of industrialising domestic satellites.

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Subject, Arirang (Multipurpose Satellite)
Subject Arirang (Multipurpose Satellite) Next-Generation Mid-Size Satellite
1 2 3 3A 5 6 7 7A 1 2
Satellite Shape 아리랑위성 1호 아리랑위성 2호 아리랑위성 3호 아리랑위성 3A호 아리랑위성 5호 아리랑위성 6호 아리랑위성 7호 아리랑위성 7a호 차세대중형위성 1호 차세대중형위성 2호
Purpose Earth observation (Optical) Precise earth observation (Optical) Precise earth observation (Optical) Precise earth observation (Optical + IR) All-weather earth observation (Image radar) All-weather earth observation (Image radar) Precise earth observation (Optical + IR) Precise earth observation (Optical + IR) Earth observation (EOS) Earth observation (EOS)
Project Period ’94.11~’00.1 ’99.12~’06.11 ’04.8~’12.8 ’06.12~’15.12 ’05.6~’15.6 '12.12 ~ '25.6 '16.8~'25.12 '20.2~'27.5 '15~'21 '18.1~'25.12
Weight(kg) 470kg 800kg 980kg Around 1,100kg Around 1,400Kg 1,750kg 2000kg 2000kg 500kg class 500kg class
Mission Life 3 years 3 years 4 years 4 years 5 years 5 years 5 years 5 years 4 years 4 years
Performance (resolution) B&W 6.6m B&W 1m
Color 4m
B&W 0.7m
Color 2.8m
B& 0.55m
Color 2.2m
Radar image 1m/3m/20m Radar image 0.5m/3m/20m B&W 0.3m
Color 1.12m
B&W 0.3,
Color < 1.12m
B&W 0.5m
Color 2m
B&W 0.5m
Color 2m
Launch Vehicle Taurus(US) Rockot(Russia) H2-A(Japan) Dnepr(Russia) Dnepr(Russia) Vega-C(France) Vega-C(France) Falcon9(US) Soyuz-2(Russia) -
Launch Site Vandenberg(US) Plesetsk(Russia) Tanegashima(Japan) Yasny(Russia) Yasny(Russia) Guyana(France) Guyana(France) Cape Canaveral(US) Baikonur (Kazakhstan) -
Launch Date ‘99.12.21 ‘06.7.28 ‘12.5.18 ‘15.3.26 ‘13.8.22 To Be Determined ‘25.10(To Be Determined) To Be Determined ‘21.3.22 To Be Determined
Operation Status Mission completed (2007.12) Mission completed (2015.10) In operation In operation In operation Under development Under development Under development In operation Under development
02

World-class satellite development technology

Although Korea was a latecomer, having begun developing satellites in the 1990s, it has come a long way thanks to continuous investment and R&D, and it is considered to be among the world's top six or seven in terms of satellite development capability. It has secured the world's most advanced satellite design, analysis, assembly, and test technologies to meet various domestic satellite demands. Having constructed a cutting-edge satellite testing facility, it owns satellite operation infrastructure and technology and satellite information utilization technology essential for satellite development.
KARI has accumulated technologies for developing low-orbit earth observation satellites and geostationary satellites applying advanced technologies through world-class satellite research and development. It transfers its satellite development technologies to private industries.

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공공 정지궤도위성 구분(천리안1호, 천리안2A호, 천리안2B호, 천리안3호)에 대한 표입니다.
Type Public geostationary orbital satellite
Cheollian 1 Cheollian 2A Cheollian 2B Cheollian 3
Shape 천리안1호 천리안2A호 천리안2B호 천리안3호
Purpose Public communication/Marine/Weather observation Weather/Spaceobservation Marine/Environmentalobservation Offering public satellite
communication service
Development Period ’03.9∼’10.12 ’11.7∼’20.10 '21.4~'27.12
Launch Date ’10.6.27 ’18.12.5 ’20.2.19 To be Determined
Weight 2,460kg 3,507kg 3,386kg 3,500kg
Life 7 years 10 years 10 years 15 years
Satellite body development AAstrium(France)/KARI
joint development
KARI KARI KARI
Launch vehicle Ariane5(France) Ariane5(France) Ariane5(France) -
Launch site Guyana(France) Guyana(France) Guyana(France) -
Remarks Korea’s first geostationary orbital satellite Geostationary orbital satellites independently developed in KOREA
Operation Status Weather observation
Mission completed (‘20.4.1)
In operation In operation Under development
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