Names | Science and Technology Satellite-2B |
---|---|
Mission type | Technology, Science |
Operator | Korea Aerospace Research Institute (KARI) |
Mission duration | 2 years (planned)[1] Failed to orbit |
Spacecraft properties | |
Spacecraft type | STSat |
Bus | STSat-2A |
Manufacturer | KAIST Satellite Technology Research Center (SaTReC) |
Launch mass | 100 kg (220 lb) [2] |
Dimensions | 62 cm x 70 cm x 90 cm |
Power | 160 watts |
Start of mission | |
Launch date | 10 June 2010, 08:01 UTC[3] |
Rocket | Naro-1 # 2 |
Launch site | Naro Space Center |
Contractor | Khrunichev / KARI |
End of mission | |
Last contact | Failed to orbit |
Orbital parameters | |
Reference system | Geocentric orbit[2] |
Regime | Low Earth (planned) |
Perigee altitude | 300 km (190 mi) |
Apogee altitude | 1,500 km (930 mi) |
Inclination | 80.0° |
Period | 103.0 minutes |
Instruments | |
Dual-channel Radiometers for Earth and Atmosphere Monitoring (DREAM) Laser Retroreflector Array (LRA) Dual Head Star Tracker (DHST) Pulsed Plasma Thruster (PPT) Fine Digital Sun Sensor (FDSS) | |
STSat-2B, or Science and Technology Satellite-2B, was a South Korean satellite which was lost in the failure of the second flight of the Naro-1 launch vehicle. It was to have been operated by the Korea Aerospace Research Institute (KARI), and was intended to demonstrate technology for future spacecraft. The satellite had a mass of 100 kg (220 lb),[2] and was expected to operate for at least two years.[1]
STSat-2B was originally intended to operate alongside a second spacecraft, STSat-2A; however STSat-2A was lost in 2009 after the payload fairing of its carrier rocket failed to separate, leaving the rocket unable to achieve orbit.[4]
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