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TDRS-8

TDRS-8, known before launch as TDRS-H, is an American communications satellite, of second generation, which is operated by NASA as part of the Tracking and Data Relay Satellite System. It was constructed by Boeing and is based on the BSS-601 satellite bus.

TDRS-8
TDRS-H undergoing processing before launch
Mission typeCommunication
OperatorNASA
COSPAR ID2000-034A
SATCAT no.26388
Mission durationPlanned: 11 years
Elapsed: 23 years, 9 months, 10 days
Spacecraft properties
BusBSS-601
ManufacturerBoeing
Launch mass3197 kg
Dimensions21.0 metres long
13.1 metres wide
Power2300 watts
Start of mission
Launch date30 June 2000, 12:56:00 (2000-06-30UTC12:56) UTC
RocketAtlas IIA
Launch siteCape Canaveral, LC-36A
ContractorILS
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Longitude171.0° West (2000-?)
270.8° West
Epoch1 July 2000
 

Launch edit

 
The launch of TDRS-H

Its launch was contracted by International Launch Services, using an Atlas IIA launch vehicle. The launch occurred on 30 June 2000, at 12:56:00 UTC from Launch Complex 36A at the Cape Canaveral Air Force Station.

It was the first Tracking and Data Relay Satellite, of second generation, to be launched. Due to a malfunction of the multiple-access phased array antenna the spacecraft did not provide the expected level of performance for eighteen of the communications services that it was to provide. The same problem was found and corrected on the TDRS-9 and TDRS-10 satellites prior to their launches.

Orbit edit

Following its launch, it raised itself into geostationary orbit by means of its onboard R-4D apogee motor, and was positioned at 150.0° West for on-orbit testing. After testing was complete, it was moved to 171.0° West from where it provides communications services to spacecraft in Earth orbit, including the Space Shuttle and International Space Station.

 
Location of TDRS as of 26 May 2020
 
Location of TDRS as of 18 March 2019

See also edit

External links edit

  • Krebs, Gunter. "TDRS-8, 9, 10". Gunter's Space Page. Retrieved 3 May 2009.
  • McDowell, Jonathan (29 May 2000). . Jonathan's Space Report. Archived from the original on 6 December 2012. Retrieved 3 May 2009.
  • "TDRS-8". Failures. Sat-ND. Retrieved 3 May 2009.
  • . Advanced Technologies, Volume 8 Number 5. NASA Aerospace Technology Innovation. September 2000. Archived from the original on 31 October 2004. Retrieved 3 May 2009.


tdrs, this, article, needs, additional, citations, verification, please, help, improve, this, article, adding, citations, reliable, sources, unsourced, material, challenged, removed, find, sources, news, newspapers, books, scholar, jstor, january, 2014, learn,. This article needs additional citations for verification Please help improve this article by adding citations to reliable sources Unsourced material may be challenged and removed Find sources TDRS 8 news newspapers books scholar JSTOR January 2014 Learn how and when to remove this template message TDRS 8 known before launch as TDRS H is an American communications satellite of second generation which is operated by NASA as part of the Tracking and Data Relay Satellite System It was constructed by Boeing and is based on the BSS 601 satellite bus TDRS 8TDRS H undergoing processing before launchMission typeCommunicationOperatorNASACOSPAR ID2000 034ASATCAT no 26388Mission durationPlanned 11 yearsElapsed 23 years 9 months 10 daysSpacecraft propertiesBusBSS 601ManufacturerBoeingLaunch mass3197 kgDimensions21 0 metres long13 1 metres widePower2300 wattsStart of missionLaunch date30 June 2000 12 56 00 2000 06 30UTC12 56 UTCRocketAtlas IIALaunch siteCape Canaveral LC 36AContractorILSOrbital parametersReference systemGeocentric orbitRegimeGeostationary orbitLongitude171 0 West 2000 270 8 WestEpoch1 July 2000 Contents 1 Launch 2 Orbit 3 See also 4 External linksLaunch edit nbsp The launch of TDRS HIts launch was contracted by International Launch Services using an Atlas IIA launch vehicle The launch occurred on 30 June 2000 at 12 56 00 UTC from Launch Complex 36A at the Cape Canaveral Air Force Station It was the first Tracking and Data Relay Satellite of second generation to be launched Due to a malfunction of the multiple access phased array antenna the spacecraft did not provide the expected level of performance for eighteen of the communications services that it was to provide The same problem was found and corrected on the TDRS 9 and TDRS 10 satellites prior to their launches Orbit editFollowing its launch it raised itself into geostationary orbit by means of its onboard R 4D apogee motor and was positioned at 150 0 West for on orbit testing After testing was complete it was moved to 171 0 West from where it provides communications services to spacecraft in Earth orbit including the Space Shuttle and International Space Station nbsp Location of TDRS as of 26 May 2020 nbsp Location of TDRS as of 18 March 2019See also edit nbsp Spaceflight portal2000 in spaceflight List of TDRS satellitesExternal links editKrebs Gunter TDRS 8 9 10 Gunter s Space Page Retrieved 3 May 2009 McDowell Jonathan 29 May 2000 Issue 427 Jonathan s Space Report Archived from the original on 6 December 2012 Retrieved 3 May 2009 TDRS 8 Failures Sat ND Retrieved 3 May 2009 Communications Satellite Serves Space Projects Advanced Technologies Volume 8 Number 5 NASA Aerospace Technology Innovation September 2000 Archived from the original on 31 October 2004 Retrieved 3 May 2009 nbsp This article about one or more spacecraft of the United States is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title TDRS 8 amp oldid 1186469860, wikipedia, wiki, book, books, library,

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