Engineering:KITSAT-3 (satellite)

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Short description: South Korean satellite
KITSAT-3
NamesUribyol-3
Mission typeTechnology demonstration, Remote sensing
OperatorSaTReC
COSPAR ID1999-029A
SATCAT no.25757
WebsiteKAIST SaTReC
Mission duration3 years (planned)
4.5 years (achieved)
Spacecraft properties
SpacecraftKITSAT-3
ManufacturerSaTReC
Launch mass110 kg (240 lb)
Dimensions49.5 cm × 60.4 cm × 85.2 cm (19.5 in × 23.8 in × 33.5 in)
Power180 watts
Start of mission
Launch date26 May 1999, 06:22 UTC
RocketPSLV-C2
Launch siteSatish Dhawan Space Centre,
ContractorIndian Space Research Organisation (ISRO)
End of mission
DeactivatedDecember 2003
Orbital parameters
Reference systemGeocentric orbit
RegimeSun-synchronous orbit
Instruments
Multispectral Earth Imaging System (MEIS)
Space ENvironment Scientific Experiment (SENSE)
STSat-1 →
 

KITSAT-3 was a South Korean remote sensing minisatellite which carried MEIS (Multispectral Earth Imaging System) and SENSE (Space ENvironment Scientific Experiment) instruments to low Earth orbit (LEO). Launched on 26 May 1999 by Indian space agency Indian Space Research Organisation (ISRO), on orbit the satellite was renamed to Uribyol-3. Manufactured by KAIST Satellite Technology Research Center (SaTReC), KITSAT-3 was developed with experience from KITSAT-1 and KITSAT-2 (no heritage to the KITSAT-1 and KITSAT-2 bus) and was the first independently designed South Korean satellite.[1][2][3][4]

Launch

Kitsat-3 was launched in the PSLV-C2 mission by 26 May 1999 by Indian space agency ISRO at 06:22 UTC from Satish Dhawan Space Centre in India. The launch was the first commercial launch by ISRO of its launch vehicle (PSLV-C2) and US$1.0 million (equivalent to US$1.53 million in 2019) was charged by the Indian agency for launching and injecting the satellite in the low Earth orbit.[5]

Mission highlights

  • First independently designed South Korea n satellite
  • First commercial flight of the launch vehicle, Polar Satellite Launch Vehicle (PSLV)
  • Spacecraft attitude was first captured and 3-axis stabilized on 30 May 1999
  • First image obtained on 31 May 1999
  • Solar panels deployed on 24 June 1999
  • Design for life of 3 years
  • However, operations ended in December 2003 (4.5 years achieved) [1][2][3][4]

See also

References