Olympus-1was acommunications satellitebuilt byAstrium(at the time of the construction of the satelliteBritish AerospaceandMatra Marconi Space) andThales Alenia Space(also at the time Alcatel Espace and Alenia Spazio), along withFokkerandSPAR Aerospace,for theEuropean Space Agency.At the time of its launch on 12 July 1989, it was the largest civilian telecommunications satellite ever built, and sometimes known as "LargeSat" or "L-Sat". The satellite had a series of unfortunate accidents in orbit and went out of service on 11/12 August 1993.[1]The first accident was the loss of ability to articulate the satellite's solar arrays. This was later followed by the loss of an on-board gyro during the height of thePerseidsmeteor shower. The satellite spun out of control and efforts to stabilise it resulted in the expenditure of the majority of its fuel. Subsequently, it was moved to a GEOdisposal orbitand was put out of commission.[2]The Olympus bus was reincarnated asAlphabus,made by the same manufacturers, this time forInmarsat(Inmarsat-4A F4).

Olympus-1
Mission typeCommunication, experimental
OperatorESA
COSPAR ID1989-053AEdit this at Wikidata
SATCATno.20122
Mission duration4 years, 1 month
Spacecraft properties
BusL-Sat
ManufacturerAstrium
Thales Alenia Space
Launch mass2,612 kilograms (5,758 lb)[1]
Power3600 watts
Start of mission
Launch date12 July 1989(1989-07-12)
RocketAriane 3,V32
Launch siteGuiana Space Centre
Kourou,French Guiana
ContractorArianespace
End of mission
DisposalDecommissioned
Deactivated12 August 1993(1993-08-13)
Orbital parameters
Reference systemGeocentric
RegimeGeostationary

References

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  1. ^ab"ESA Achievements BR-200 - Olympus"(PDF).ESA.November 2001. Archived fromthe original(PDF)on 30 September 2007.Retrieved18 February2019.
  2. ^"Shooting Stars Can Shoot Down Satellites".IEEE.31 March 2010.Retrieved7 February2012.
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