Mission type | Communication |
---|---|
Operator | NASA |
COSPAR ID | 1995-035B |
SATCAT no. | 23613 |
Mission duration | Planned: 10 years Elapsed: 29 years |
Spacecraft properties | |
Bus | TDRS |
Manufacturer | TRW |
Launch mass | 2,108 kilograms (4,647 lb) [1] |
Dimensions | 17.3 metres (57 ft) long 14.2 metres (47 ft) wide |
Power | 1700 watts |
Start of mission | |
Launch date | 13 July 1995, 13:41:55 UTC |
Rocket | Space Shuttle Discovery STS-70 / IUS |
Launch site | Kennedy Space Center, LC-39B |
Contractor | Rockwell International |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 150.0° West (1995–1996) 171.0° West (1996–2003) 150.5° West (2003–) |
Epoch | 14 July 1995 [2] |
TDRS-7, known before launch as TDRS-G, is an American communications satellite, of first generation, which is operated by NASA as part of the Tracking and Data Relay Satellite System. It was constructed by TRW as a replacement for TDRS-B, which had been lost in the Challenger accident, and was the last first generation TDRS satellite to be launched.
TDRS-7 is based on a custom satellite bus which was used for all seven first generation TDRS satellites. [3] Whilst similar to its predecessors, it differed from them slightly in that twelve G/H band (C band (IEEE)) transponders which had been included on the previous satellites were omitted. [4] It was the last communications satellite, other than amateur radio spacecraft, to be deployed by a Space Shuttle.
The TDRS-G satellite was deployed from Space Shuttle Discovery during the STS-70 mission in 1995. Discovery was launched from Kennedy Space Center Launch Complex 39B at 13:41:55 UTC on 13 July 1995. [5] TDRS-G was deployed from Discovery around six hours after launch, and was raised to geosynchronous orbit by means of an Inertial Upper Stage. [5]
The twin-stage solid-propellent Inertial Upper Stage made two burns. The first stage burn occurred around an hour after deployment from Discovery, and placed the satellite into a geosynchronous transfer orbit. At 02:30 UTC on 14 July 1995 it reached apogee, and the second stage fired, placing TDRS-G into geostationary orbit. [6] At this point, it received its operational designation, TDRS-7. It was placed at a longitude 150.0° West of the Greenwich Meridian, where it underwent on-orbit testing. In May 1996, it was moved to 171.0° West where it was stored as an in-orbit spare, and subsequently entered service. [7] In December 2003, it was relocated to 150.5° West. [8] It arrived the next month, and was returned to storage as a reserve satellite.
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