Content deleted Content added
No edit summary |
|||
Line 1:
{{Use mdy dates|date=April 2014}}
[[File:TDRS Heart of Communication.ogv|thumb|350px|The launch of TDRS-K begins the replenishment of the fleet through the development and deployment of the next generation spacecraft.]]
[[File:Tracking Data Relay Satellite (TDRS) Orbital Fleet Communicating with User Spacecraft.ogg|thumb|350px|This visualization begins by showing how a typical spacecraft (NIMBUS-7) communicated with the ground before TDRS.]]
A '''tracking and data relay satellite''' ('''TDRS''') is a type of [[communications satellite]] that forms part of the [[TDRSS|Tracking and Data Relay Satellite System]] (TDRSS) used by [[NASA]] and other
The first seven TDRSS satellites were built by the [[TRW Inc.|TRW]] corporation. The three later versions have been manufactured by the [[Boeing]] corporation's [[Boeing Satellite Systems|Satellite Systems]] division. Ten satellites have been launched; however, one was destroyed in a launch failure (the [[Challenger disaster]]). TDRS-1 was decommissioned in October 2009.<ref name=T1decomm>{{cite web|url=http://spaceflightnow.com/news/n0910/13tdrs/ |title=Breaking News | NASA retires 'queen' of tracking satellite fleet |publisher=Spaceflight Now |date= |accessdate=February 5, 2014
==Operations==
The first tracking and data relay satellite was launched in 1983 on the [[Space Shuttle Challenger|Space Shuttle ''Challenger's'']] first flight, [[STS-6]]. The Boeing-built [[Inertial Upper Stage]] that was to take the satellite from Challenger's orbit to its ultimate [[geosynchronous orbit]] suffered a failure that caused it not to deliver the TDRS to the correct orbit. As a result, it was necessary to command the satellite to use its onboard [[Reaction control system|rocket thrusters]] to move it into its correct orbit. This expenditure of fuel reduced its capability to remain in a [[geostationary]] orbit; by late 1997 the orbit had changed to the point that the satellite was able to see the South Pole, and an uplink/downlink station was installed at [[Amundsen-Scott South Pole Station]] in January 1998;<ref name=southpole>{{cite web |url=http://antarcticsun.usap.gov/features/contentHandler.cfm?id=1742 |title=TDRS history |date=
The second tracking and data relay satellite was destroyed along with ''Challenger'' shortly after launch during the [[STS-51-L]] mission in January 1986. The next five TRW-built TDRSS satellites were successfully launched on other Space Shuttles. Three follow-up Boeing-built satellites were launched by [[Atlas rocket]]s in 2000 and 2002. A NASA Press Release<ref>{{cite web|url=http://www.nasa.gov/home/hqnews/2003/apr/HP_news_03130.html |title=NASA
<blockquote>"Working solo, TDRS-1 provided more communication coverage, in support of the September 1983 Shuttle mission, than the entire network of NASA tracking stations had provided in all previous Shuttle missions."</blockquote>
The first generation of TDRS are planned to be retired in 2015.<ref name=NASA>{{cite web|url=http://www.nasa.gov/home/hqnews/2011/nov/HQ_C11-049_TDRS.html|title=NASA Exercises Contract Option For TDRS-M Satellite Decision Will Retain Hundreds
==TDRSS ground terminals==
The two [[TDRSS#Ground segment|TDRSS satellite ground terminal]]s are located at NASA White Sands Complex, which is in the [[Las Cruces, New Mexico|Las Cruces]] area. All radioed commands and received [[telemetry]] that go to and from the tracking and data relay satellites go by way of these terminals at the White Sands Complex. At first, just one large ground terminal system for the TDRSS was designed and built. However, some years later, due to increased user demand [[NASA]] ordered the design and construction of a second ground terminal system about {{convert|5|km}} away. Thus, there are now two functionally identical and redundant satellite ground terminals there, which are known as the [[White Sands Complex]]. Due to a Zone of Exclusion, no user support over the
=== Bilateration ranging transponder system ===
The bilateration ranging transponder system (BRTS) provides tracking support for TDRS spacecraft. BRTS consists of four sites located at [[White Sands Missile Range]] (WSC), [[American Samoa]] (AMS), [[Ascension Island]] (ACN), and [[Alice Springs]],
==Design==
The communications systems of the TDRSS satellites were designed to support multiple missions at the same time. Each satellite has [[S band]], [[Ku band|K<sub>u</sub> band]] (1st Gen only), and [[Ka band|K<sub>a</sub> band]] (2nd gen only) electronic communication systems hardware that operate at different carrier frequencies and also support various data-rates.<ref>{{cite web|url=http://www.nasa.gov/centers/goddard/pdf/97440main_TDRS_fs_9.18.pdf |title= NASA Goddard TDRS Radio Frequency Systems (need Adobe Acrobat Reader)|publisher=Nasa.gov|accessdate=February 5, 2014
==Different versions of the TDRS ==
: ''Section source: NASA TDRSS official site''<ref>{{cite web|url=https://www.spacecomm.nasa.gov/spacecomm/programs/tdrss/default.cfm |title=Tracking and Data Relay Satellite (TDRS) | NASA |publisher=Spacecomm.nasa.gov |date=
*First Generation TDRS: models A to G
*Second Generation TDRS: models H to J
*Third Generation TDRS: models K to L (M and N are planned)<ref>{{cite web|url=http://space.skyrocket.de/doc_sdat/tdrs-11.htm |title=TDRS 11, 12, 13 (TDRS K, L, M) |publisher=Space.skyrocket.de |date= |accessdate=February 5, 2014
*Launch Site: [[Cape Canaveral]], United States
*Launch Vehicle: [[Space shuttle]], [[Atlas II]] or [[Atlas V]] booster
Line 40 ⟶ 41:
===TDRS background===
:''Source: NASA: TDRS A Satellite''<ref name=tdrsa>{{cite web|url=http://nssdc.gsfc.nasa.gov/nmc/spacecraftDisplay.do?id=1983-026B |title=NASA
TDRS-A was the first of TDRSS multiple satellite tracking system. The system is a concept utilizing communication satellite technology that improves and economizes the satellite tracking and [[telemetry]] operations. The base three [[geosynchronous satellites]] (one a standby) track and receive data from satellites for relay to a ground station. The two primary active satellites are separated in orbit by at least 130 degrees longitude.
|