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GOES 8

From Wikipedia, the free encyclopedia
NOAA weather satellite
GOES-8
Artist's impression of a GOES-I series satellite in orbit
Mission typeWeather satellite
OperatorNOAA / NASA
COSPAR ID1994-022AEdit this at Wikidata
SATCATno.23051
Mission duration3-5 years (planned)
10 years (achieved)
Spacecraft properties
BusLS-1300
ManufacturerSpace Systems/Loral
Launch mass2,105 kilograms (4,641 lb)
Start of mission
Launch date13 April 1994, 06:04 (1994-04-13UTC06:04Z) UTC
RocketAtlas I
Launch siteCape CanaveralLC-36B
ContractorMartin Marietta
End of mission
DisposalDecommissioned
Deactivated5 May 2004 (2004-05-06)
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Longitude75° West
SlotGOES-EAST (1995-2003)
Eccentricity0.0005384
Perigee altitude36,151 kilometres (22,463 mi)
Apogee altitude36,197 kilometres (22,492 mi)
Inclination10.89°
Period1,456.0 minutes

GOES-8, known asGOES-I before becoming operational, was an Americanweather satellite, which formed part of the USNational Oceanic and Atmospheric Administration'sGeostationary Operational Environmental Satellite system. It was launched in 1994, and operated until 2004 when it was retired and boosted to agraveyard orbit.[1][2] At launch, the satellite had a mass of 2,105 kilograms (4,641 lb), and an expected operational lifespan of three or five years.[3][4] It was built bySpace Systems/Loral, based on theLS-1300 satellite bus, and was the first of five GOES-I series satellites to be launched.

Launch

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GOES-I was launched aboard aMartin MariettaAtlas I rocket, flying fromLaunch Complex 36B at theCape Canaveral Air Force Station.[5] The launch occurred at 06:04 GMT on 13 April 1994,[5] and placed the satellite into ageosynchronous transfer orbit. It was then raised intogeostationary orbit by means of anR-4D-11apogee motor.[3] During the first burn of the apogee motor, an unusually high temperature was detected in one of theflanges upon which a thruster was mounted,[6] however later analysis, based on satellites using similar thruster systems, demonstrated that it was still acceptable.[6] During the third burn, a malfunction of the computer controlling the attitude control system caused several manoeuvring thrusters to fire. This resulted in the burn being aborted.[6]

GOES-8 was eventually raised to the correct orbit, and positioned at alongitude of 75° West.[4][7] Following on-orbit testing, it was activated as the GOES-EAST satellite, allowingGOES-7, which had previously been covering both positions, to assume GOES-WEST operations.

Operations

[edit]
The first image returned by GOES-8

GOES-8 suffered from a design fault with the motor windings in its imager and sounder, with one of two sets failing within a few years of it becoming operational. If the other set had failed, it would have made the system inoperable. This fault also occurred on theGOES-9 satellite, which was launched in 1995. It was corrected beforeGOES-10 was launched.[8] In 1997, one of its momentum wheels failed, however unlike with GOES-9, the other wheel was not affected, and the satellite was able to continue operations.[4] GOES-8 was also featured in the 1996 filmTwister.

GOES-8 was retired from GOES-EAST operations in 2003, when it was replaced byGOES-12.[9] Following this it remained in storage for a year as a backup, before being boosted to agraveyard orbit between 4 and 5 May 2004.[4]

See also

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References

[edit]
  1. ^"GOES-NEWS". NASA. 2009-05-09. Archived fromthe original on 2004-06-05. Retrieved2009-07-13.
  2. ^"GOES-8 Spacecraft Status Summary". NOAA. Archived fromthe original on 2006-08-18. Retrieved2009-07-13.
  3. ^abKrebs, Gunter."GOES-8, 9, 10, 11, 12". Gunter's Space Page. Retrieved2009-07-13.
  4. ^abcd"GOES-I Status". NOAA. Archived fromthe original on 2004-07-04. Retrieved2009-07-11.
  5. ^abMcDowell, Jonathan."Launch Log". Jonathan's Space Page. Retrieved2009-07-13.
  6. ^abcHarland, David M; Lorenz, Ralph D. (2005).Space Systems Failures (2006 ed.). Chichester: Springer-Praxis. pp. 194–195.ISBN 0-387-21519-0.
  7. ^Wade, Mark."GOES-Next". Encyclopedia Astronautica. Archived fromthe original on February 21, 2002. Retrieved2009-07-11.
  8. ^"GOES Motor Windings". NASA. 2001-04-27. Archived fromthe original on 2004-07-13. Retrieved2009-07-11.
  9. ^"GOES-8/12 Transition Plan"(PDF). NASA. 2002-10-28. Archived fromthe original(PDF) on 2004-10-30. Retrieved2009-07-09.
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