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This is an old revision of this page, as edited by Yobot (talk | contribs)at15:58, 31 January 2015 (Replace obsolete <br> tag attributes per Wikipedia:HTML5#Other_obsolete_attributes and/or other changes using AWB (10811)). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.
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TDRS-5, known before launch as TDRS-E, is an American communications satellite which is operated by NASA as part of the Tracking and Data Relay Satellite System. It was constructed by TRW is based on a custom satellite bus which was used for all seven first generation TDRS satellites.[2]

TDRS-5
TDRS-E aboard Atlantis during deployment
Mission typeCommunication
OperatorNASA
COSPAR ID1991-054B Edit this at Wikidata
SATCAT no.21639Edit this on Wikidata
Mission duration7 years (planned)
18+ years (achieved)
Spacecraft properties
ManufacturerTRW
Launch mass2,268 kilograms (5,000 lb)
Start of mission
Launch date2 August 1991, 15:02:00 (1991-08-02UTC15:02Z) UTC
RocketSpace Shuttle Atlantis
STS-43 / IUS
Launch siteKennedy LC-39A
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Longitude174° West[1]
 

History

 
The launch of STS-43, carrying TDRS-5

It was launched aboard Space Shuttle Atlantis during the STS-43 mission in August 1991. Atlantis launched from Launch Complex 39A at the Kennedy Space Center at 15:02:00 GMT (11:02 local time), on 2 August.[3] TDRS-E was deployed from Atlantis around six hours after launch, and was raised to geostationary orbit by means of an Inertial Upper Stage. It was the only TDRS satellite to be deployed from Atlantis.[3]

Deployment

The twin-stage solid-propellent Inertial Upper Stage made two burns. The first stage burn occurred shortly after deployment, from Atlantis, and placed the satellite into a geosynchronous transfer orbit. Around six hours later, it reached apogee, and the second stage fired, placing TDRS-E into geosynchronous orbit. At this point it received its operational designation, TDRS-5. It was placed at a position over the equator, 174° West of the Greenwich Meridian,[1] from where it provides communications services to spacecraft in Earth orbit, including the Space Shuttle and International Space Station. Some of its transponders are operated by the Columbia Communications Corporation.[4]

References

  1. ^ a b "The TDRS-J satellite". Spaceflight Now. 2002-12-01. Retrieved 2009-08-02.
  • ^ Krebs, Gunter. "TDRS 1, 2, 3, 4, 5, 6". Gunter's Space Page. Retrieved 2009-08-02.
  • ^ a b McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 2009-08-02.
  • ^ "TDRS 5". TSE. Retrieved 2009-08-02.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=TDRS-5&oldid=645000485"
     



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    This page was last edited on 31 January 2015, at 15:58 (UTC).

    This version of the page has been revised. Besides normal editing, the reason for revision may have been that this version contains factual inaccuracies, vandalism, or material not compatible with the Creative Commons Attribution-ShareAlike License.



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