Engineering:KOMPSAT-2

From HandWiki
Revision as of 17:17, 4 February 2024 by QCDvac (talk | contribs) (update)
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)
KOMPSAT-2
NamesKorean Multi-purpose Satellite-2
Arirang-2
Mission typeEarth observation
OperatorKorea Aerospace Research Institute
COSPAR ID2006-031A
SATCAT no.29258
Mission duration3 years (planned)
18 years, 4 months and 22 days (in progress)
Spacecraft properties
Spacecraft typeKOMPSAT
ManufacturerKorea Aerospace Industries
Korea Aerospace Research Institute
EADS Astrium (bus)
Launch mass800 kg (1,800 lb)
Dimensions1.85 m diameter x 2.6 m in height x 6.8 m length (deployed configuration)
Power955 watts
Start of mission
Launch date28 July 2006, 07:05:43 UTC
RocketRokot-KM
Launch sitePlesetsk, Site 133/3
ContractorKhrunichev State Research and Production Space Center
Orbital parameters
Reference systemGeocentric orbit[1]
RegimeSun-synchronous orbit
Altitude685 km (426 mi)
Inclination98.13°
Period98.46 minutes
Instruments
Multispectral Camera (MSC)
KOMPSAT programme
 

KOMPSAT-2 (Korean Multi-purpose Satellite-2), also known as Arirang-2,[2] is a South Korean multipurpose Earth observation satellite. It was launched from Plesetsk Cosmodrome, Russia at 07:45:43 UTC (16:05:43 KST) on 28 July 2006. It began to transmit signals at 14:00 UTC (23:00 KST) the same day. Like the earlier KOMPSAT-1 satellite, it takes its name from the popular Korean folk song Arirang. Its launch was the culmination of a project begun in 1995.[3]

KOMPSAT-2 orbits at a height of 685 km (426 mi), circling the Earth 14 times per day, and is expected to maintain that orbit for 3 years. It weighs 800 kg (1,800 lb).[4] The satellite carries a Multispectral Camera (MSC) which can distinguish to a 100-cm resolution, allowing the identification of individual vehicles on the ground.[5] The satellite was succeeded by KOMPSAT-3, KOMPSAT-5 and KOMPSAT-3A, which were launched in 2012, 2013 and 2015 respectively.

History

South Korea started the KOMPSAT programme in 1995 to nurture its national Earth-imaging industry and supply services for remote-sensing applications. The South Korean KOMPSAT-2 Earth-imaging satellite was developed by Korea Aerospace Industries (KAI) and Korea Aerospace Research Institute (KARI), in partnership with EADS Astrium, to assure continuity with the KOMPSAT-1 satellite launched in 1999. KOMPSAT-2 was orbited on 28 July 2006 by a launch vehicle from Plesetsk, Russia. Spot Image was the distributor of KOMPSAT-2 imagery until April 2011. SI Imaging Services is the worldwide exclusive distributor of KOMPSAT imagery including KOMPSAT-2 since November 2012.

Technologies

Orbit

KOMPSAT-2 operates in a near-polar, circular Sun-synchronous orbit. The orbital parameters are:

  • Mean altitude: 685 km
  • Mass: 800 kg
  • Inclination: 98.1° (Sun-synchronous orbit)
  • Orbital period: 98.6 minutes
  • Orbital cycle: 28 days

Instruments

KOMPSAT-2's instruments are designed to acquire high- and very-high-resolution imagery with a footprint of 15 km. The satellite has the capacity to acquire 20 minutes of imagery on each orbit and it can steer its sensors both ways out to 30° off track. Panchromatic and multispectral images can be acquired at the same time.

KOMPSAT-2 radiometer features:

Kompsat-2 radiometric parameters
mode Channel Spectral band Spatial resolution Footprint
Multispectral 1 0.45 - 0.52 μm (blue) 4 m 15 km
2 0.52 - 0.60 μm (green) 4 m 15 km
3 0.63 - 0.69μm (rouge) 4 m 15 km
4 0.76 - 0.90 μm (near-infrared) 4 m 15 km
Panchromatic P 0.50 - 0.90 μm (black and white) 1 m 15 km

Ground receiving stations

Two receiving stations deliver KOMPSAT-2 imagery 1 to 3 days after acquisition and in under 24 hours in Europe. The Deajeon station in South Korea is responsible for tasking the satellite. The Toulouse station in France is responsible for updating the catalogue, producing imagery and delivering it to its customers.

Advantages and applications of KOMPSAT-2 imagery

KOMPSAT-2 is designed for very-high-resolution (VHR) remote-sensing applications, such as:

  • Land planning: to detect and identify features smaller than 1 square meter, e.g. vehicles, street furnishings, roads and bushes
  • Agriculture: to pinpoint crop or tree diseases
  • Urban planning and demographics: to locate detached houses
  • Civil engineering: to plan road, railroad and oil pipeline corridors
  • Defence: to describe high-value assets or military sites

North Korea

It serves along with the existing Kompsat-2 to provide continuous satellite observation of the Korean Peninsula, sending images twice a day at 1:30 and 13:30.[6]

Mission

In October 2015, the Ministry of Science, ICT and Future Planning (MSIP) and KARI made plans about the future of the KOMPSAT-2 mission which is on orbit for more than 9 years. It was decided not to extend the KOMPSAT-2 mission any further for systematic observation services, but instead use it for research purposes until the end of its life cycle. Although KOMPSAT-2 was originally designed to have a life cycle of 3 years, this was extended three times (by two years each time, for a total of 6 years) by applying highly reliable satellite technology. KOMPSAT-2 has successfully carried out its mission of obtaining images of the Korean Peninsula and other major areas of the world over a period of nine years. KOMPSAT-2 is used in next-generation satellite technology research without any further extension of its mission until the end of its life cycle, as its operation systems - such as its payload module, sensor, and Earth station operation system (command transmission and satellite condition analysis) - are aged.[7]

See also

References

External links