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PROBA-2

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PROBA-2
Mission typeTechnology
Space weather
OperatorEuropean Space Agency[1]
COSPAR ID2009-059BEdit this at Wikidata
SATCATno.36037
Mission duration2 years (planned) 14 years, 8 months and 14 days (in progress)
Spacecraft properties
BusPROBA
ManufacturerVerhaert Design & Development (now QinetiQ Space)
Launch mass120 kilograms (260 lb)
Dimensions0.60m x 0.70m x 0.85m
Power120 watts
Start of mission
Launch date2 November 2009, 01:50:00(2009-11-02UTC01:50Z)UTC
RocketRokot/Briz-KM
Launch sitePlesetsk133/3
Orbital parameters
Reference systemGeocentric
RegimeSun-synchronous
Perigee altitude713 kilometres (443 mi)[2]
Apogee altitude733 kilometres (455 mi)[2]
Inclination98.28 degrees[2]
Period99.12 minutes[2]
Epoch24 January 2015, 13:01:08 UTC[2]
PROBA-2 mission logo
ESA solar system insignia for thePROBA-2mission

PROBA-2is the second satellite in theEuropean Space Agency's series ofPROBAlow-costsatellitesthat are being used to validate new spacecraft technologies while also carrying scientific instruments.[3]PROBA-2 is a small satellite (130 kg) developed under an ESA General Support Technology Program (GSTP) contract by a Belgian consortium led by Verhaert (nowQinetiQ Space) of Kruibeke, Belgium. The nominal mission duration was two years.[1]As of 2022, the mission continues.[4]

Mission summary[edit]

It was launched on 2 November 2009, with theRockotlaunch system together withESA'sSMOSmission.[5]The platform was launched in aSun-synchronous orbitlow Earth orbit(altitude of 725 km).[1]

PROBA-2 contains five scientific instruments. Two of them are designated to observe theSun:"The Sun Watcher using APS and Image Processing" (SWAP,an EUV imager) and the "Large Yield Radiometer" (LYRA), a radiometer made of diamond photodiodes. The Principal investigator teams of both instruments are hosted at theRoyal Observatory of Belgium.This institute will also host thePROBA-2 Science Centerfrom which theSWAPandLYRAinstruments will be operated and their data distributed. There are three other instruments to measure basic space plasma properties: theDual segmented Langmuir probe(DSLP)[1](developed by theAstronomical Instituteand Institute of Atmospheric Physics, Academy of Sciences of the Czech Republic), the Thermal Plasma Measurement Unit (TPMU), and the Science Grade Vector Magnetometer (SGVM) developed by theTechnical University of Denmark.[1]

See also[edit]

References[edit]

  1. ^abcde"PROBA-2 (Project for On-Board Autonomy-2)".ESA.Retrieved2013-04-15.
  2. ^abcde"PROBA-2 Satellite details 2009-059B NORAD 36037".N2YO. 24 January 2015.Retrieved25 January2015.
  3. ^"About PROBA-2".ESA.2012-12-02.Retrieved2013-04-15.
  4. ^"ESA Science & Technology - PROBA2".
  5. ^"Successful launch qualification test for PROBA-2".ESA.2008-09-16. Archived fromthe originalon 2011-07-25.Retrieved2013-04-15.

External links[edit]