STSat-2B

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
NamesScience and Technology Satellite-2B
Mission typeTechnology, Science
OperatorKorea Aerospace Research Institute (KARI)
Mission duration2 years (planned)[1]
Failed to orbit
Spacecraft properties
Spacecraft typeSTSat
BusSTSat-2A
ManufacturerSatellite Technology Research Center (SaTReC)
Launch mass100 kg (220 lb) [2]
Dimensions62 cm x 70 cm x 90 cm
Power160 watts
Start of mission
Launch date10 June 2010, 08:01 UTC[3]
RocketNaro-1 # 2
Launch siteNaro Space Center
ContractorKhrunichev / KARI
End of mission
Last contactFailed to orbit
Orbital parameters
Reference systemGeocentric orbit[2]
RegimeLow Earth (planned)
Perigee altitude300 km (190 mi)
Apogee altitude1,500 km (930 mi)
Inclination80.0°
Period103.0 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 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]

Instruments

The primary instrument aboard STSat-2B was the Dual-channel Radiometer for Earth and Atmosphere Monitoring, or DREAM, which would have measured the brightness temperature of the Earth at 23.8 GHz and 37 GHz.[5] The secondary payload, the Laser Retroreflector Array (LRA) was to have been used for the Satellite laser ranging experiment, which was intended to determine the parameters of the satellite's orbit with a greater degree of precision. Data collected by the secondary payload would have been used to calibrate DREAM, to conduct geodetic research, and to evaluate the performance of the launch vehicle.[1] Due to lower manufacturing tolerance, the retroreflectors on STSat-2B would have provided greater precision than those intended on STSat-2A.[6]

A series of technological experiments were also to have been conducted; investigating attitude control systems, and testing pulsed plasma thrusters, star trackers, a Sun sensor, as well as an experimental onboard computer, and data relay at rates of up to 10 megabits per second.[1]

Launch

STSat-2B was launched by a Naro-1 launch vehicle, flying from the Naro Space Center. The launch was the second flight of the Naro-1, which consisted of a modified Angara first stage manufactured by Khrunichev,[7] and a South Korean solid-fuelled upper stage. The previous Naro-1 launch was that of STSat-2A, which occurred in August 2009 and ended in failure.[4]

The launch was initially scheduled to occur on 9 June 2010, during a two-hour launch window opening at 07:30 UTC (16:30 local time). Further launch attempts were available at the same time each day until 19 June 2010.[8] The launch attempt on 9 June 2010 was scrubbed after the launch pad's fire suppression system activated for no apparent reason.

Following the scrub, the launch was rescheduled for the next day, and took place at 08:01 UTC (17:01 local time) on 10 June 2010.[3] During the first stage burn, around 137 seconds into the flight, contact with the rocket was lost.[9] South Korean science minister Ahn Byung-man later told reporters that the rocket was believed to have exploded.[10] If the launch had been successful, STSat-2B would have been deployed into an orbit with a perigee of 300 km (190 mi), an apogee of 1,500 km (930 mi), and around 80.0° of inclination.[2]

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References
  1. Noll, Carey. "ILRS Mission Support Status". STSat-2 Satellite Information. NASA. Archived from the original on 25 May 2010. Retrieved 24 April 2010. Public Domain This article incorporates text from this source, which is in the public domain.
  2. Noll, Carey. "STSat-2". STSat-2 Satellite Information. NASA. Archived from the original on 16 May 2010. Retrieved 24 April 2010. Public Domain This article incorporates text from this source, which is in the public domain.
  3. "South Korea's Naro-1 rocket lifts off from space center". Yonhap News. 10 June 2010. Retrieved 10 June 2010.
  4. Lee Joon-seung (26 August 2010). "South Korean satellite lost shortly after launch". Yonhap News. Retrieved 24 April 2010.
  5. Sung-Hyun Kim; Ho-Jin Lee; Chun-Sik Chae; Hyuk Park; Seok-Hun Yun; Jong-Oh Park; Seung-Hun Lee; Eun-Sup Sim; De-Hai Zhang; Jing-Shan Jiang; Yong-Hoon Kim (2005). "Dual-channel Radiometers for Earth and Atmosphere Monitoring(DREAM) on Micro-Satellite STSAT-2". 2005 Asia-Pacific Microwave Conference Proceedings. Vol. 1. pp. 1–3. doi:10.1109/APMC.2005.1606350. ISBN 0-7803-9433-X. S2CID 1003642.
  6. Noll, Carey. "RetroReflector Array (RRA) Characteristics". STSAT-2 Satellite Information. NASA. Archived from the original on 24 May 2010. Retrieved 24 April 2010. Public Domain This article incorporates text from this source, which is in the public domain.
  7. "First-Stage Engine of Naro-1 to Arrive on Weekend". Arirang. 2 April 2010. Archived from the original on 23 February 2012. Retrieved 24 April 2010.
  8. Jang Ji-yun (20 April 2010). "Korea to Launch 2nd Naro Space Rocket on June 9". Arirang. Archived from the original on 23 February 2012. Retrieved 24 April 2010.
  9. "Ground controllers lose contact with space rocket after takeoff". Yonhap News. 10 June 2010. Retrieved 10 June 2010.
  10. "South Korean space rocket might have exploded: science minister". Xinhua. 10 June 2010. Archived from the original on 12 June 2010. Retrieved 10 June 2010.
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