Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

STSat-2B

From Wikipedia, the free encyclopedia
Failed South Korean satellite

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
ManufacturerKAIST Satellite Technology Research Center (SaTReC)
Launch mass100 kg (220 lb)[2]
Dimensions62 cm x 70 cm x 90 cm
Power160watts
Start of mission
Launch date10 June 2010, 08:01UTC[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, orScience and Technology Satellite-2B, was a South Koreansatellite which was lost in the failure of the second flight of theNaro-1launch vehicle. It was to have been operated by theKorea Aerospace Research Institute (KARI), and was intended to demonstratetechnology 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]

Instruments

[edit]

The primary instrument aboard STSat-2B was theDual-channel Radiometer for Earth and Atmosphere Monitoring, or DREAM, which would have measured thebrightness temperature of theEarth at 23.8GHz and 37 GHz.[5] The secondary payload, the Laser Retroreflector Array (LRA) was to have been used for theSatellite 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 conductgeodetic 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; investigatingattitude control systems, and testingpulsed plasma thrusters,star trackers, aSun sensor, as well as an experimental onboard computer, and data relay at rates of up to 10megabits per second.[1]

Launch

[edit]

STSat-2B was launched by a Naro-1 launch vehicle, flying from theNaro Space Center. The launch was the second flight of the Naro-1, which consisted of a modifiedAngara first stage manufactured byKhrunichev,[7] and a South Koreansolid-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-hourlaunch window opening at 07:30UTC (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 ministerAhn 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 aperigee of 300 km (190 mi), anapogee of 1,500 km (930 mi), and around 80.0° ofinclination.[2]

References

[edit]
  1. ^abcdNoll, Carey."ILRS Mission Support Status".STSat-2 Satellite Information. NASA. Archived fromthe original on 25 May 2010. Retrieved24 April 2010.Public Domain This article incorporates text from this source, which is in thepublic domain.
  2. ^abcdNoll, Carey."STSat-2".STSat-2 Satellite Information. NASA. Archived fromthe original on 16 May 2010. Retrieved24 April 2010.Public Domain This article incorporates text from this source, which is in thepublic domain.
  3. ^ab"South Korea's Naro-1 rocket lifts off from space center".Yonhap News Agency. 10 June 2010. Retrieved10 June 2010.
  4. ^abLee Joon-seung (26 August 2010)."South Korean satellite lost shortly after launch".Yonhap News Agency. Retrieved24 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 fromthe original on 24 May 2010. Retrieved24 April 2010.Public Domain This article incorporates text from this source, which is in thepublic domain.
  7. ^"First-Stage Engine of Naro-1 to Arrive on Weekend". Arirang. 2 April 2010. Archived fromthe original on 23 February 2012. Retrieved24 April 2010.
  8. ^Jang Ji-yun (20 April 2010)."Korea to Launch 2nd Naro Space Rocket on June 9". Arirang. Archived fromthe original on 23 February 2012. Retrieved24 April 2010.
  9. ^"Ground controllers lose contact with space rocket after takeoff".Yonhap News Agency. 10 June 2010. Retrieved10 June 2010.
  10. ^"South Korean space rocket might have exploded: science minister". Xinhua. 10 June 2010. Archived fromthe original on 12 June 2010. Retrieved10 June 2010.
Organizations
Launch sites
Rocket engines
Completed development
Under development
KARI
ADD
KARI
ADD
Perigee Aerospace
Innospace
Small satellites
Reconnaissance satellites
Communication satellites
Earth observation
Geostationary
  • Chollian
CubeSats
Contractors
Astronauts
Related institutions
January
February
March
April
May
June
July
August
September
October
November
December
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Retrieved from "https://en.wikipedia.org/w/index.php?title=STSat-2B&oldid=1268127046"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp