Model of a Telstar satellite, on display at Conservatoire national des arts et métiers
|Manufacturer||Hughes, EADS Astrium, Space Systems/Loral, Airbus Defense and Space|
|Country of origin||United States|
|Bus||HS-376, AS-7000, Eurostar-2000, Spacebus-4000B3, SSL-1300|
|Regime||Medium Earth / Geostationary|
Telstar is the name of various communications satellites. The first two Telstar satellites were experimental and nearly identical. Telstar 1 launched on top of a Thor-Delta rocket on July 10, 1962. It successfully relayed through space the first television pictures, telephone calls, and telegraph images, and provided the first live transatlantic television feed. Telstar 2 launched May 7, 1963. Telstar 1 and 2--though no longer functional--still orbit the Earth.
Belonging to AT&T, the original Telstar was part of a multi-national agreement among AT&T (USA), Bell Telephone Laboratories (USA), NASA (USA), GPO (United Kingdom) and the National PTT (France) to develop experimental satellite communications over the Atlantic Ocean. Bell Labs held a contract with NASA, paying the agency for each launch, independent of success.
Six ground stations were built to communicate with Telstar, one each in the US, France, the UK, Canada, Germany and Italy. The American ground station--built by Bell Labs--was Andover Earth Station, in Andover, Maine. The main British ground station was at Goonhilly Downs in southwestern England. The BBC, as international coordinator, used this location. The standards 525/405 conversion equipment (filling a large room) was researched and developed by the BBC and located in the BBC Television Centre, London. The French ground station was at Pleumeur-Bodou ( ) in north-western France. The Canadian ground station was at Charleston, Nova Scotia. The German ground station was at Raisting in Bavaria. The Italian ground station was at Fucino in Abruzzo.
The satellite was built by a team at Bell Telephone Laboratories that included John Robinson Pierce, who created the project;Rudy Kompfner, who invented the traveling-wave tube transponder that the satellite used; and James M. Early, who designed its transistors and solar panels. The satellite is roughly spherical, measures 34.5 inches (876.30 mm) in length, and weighs about 170 pounds (77 kg). Its dimensions were limited by what would fit on one of NASA's Delta rockets. Telstar was spin-stabilized, and its outer surface was covered with solar cells capable of generating 14 watts of electrical power.
The original Telstar had a single innovative transponder that could relay data, a single television channel, or multiplexed telephone circuits. Since the spacecraft spun, it required an array of antennas around its "equator" for uninterrupted microwave communication with Earth. An omnidirectional array of small cavity antenna elements around the satellite's "equator" received 6 GHz microwave signals to relay back to ground stations. The transponder converted the frequency to 4 GHz, amplified the signals in a traveling-wave tube, and retransmitted them omnidirectionally via the adjacent array of larger box-shaped cavities. The prominent helical antenna received telecommands from a ground station.
Launched by NASA aboard a Delta rocket from Cape Canaveral on July 10, 1962, Telstar 1 was the first privately sponsored space launch. A medium-altitude satellite, Telstar was placed in an elliptical orbit completed once every 2 hours and 37 minutes, inclined at an angle of approximately 45 degrees to the equator, with perigee about 952 kilometres (592 mi) from Earth and apogee about 5,933 kilometres (3,687 mi) from Earth This is in contrast to the 1965 Early Bird Intelsat and subsequent satellites that travel in circular geostationary orbits.
Due to its non-geosynchronous orbit, similar to a Molniya orbit, Telstar's availability for transatlantic signals was limited to the 20 minutes in each 2.5-hour orbit when the satellite passed over the Atlantic Ocean. Ground antennas had to track the satellite with a pointing error of less than 0.06 degrees as it moved across the sky at up to 1.5 degrees per second.
Since the transmitters and receivers on Telstar were not powerful, ground antennas had to be huge. Bell Laboratory engineers designed a large horizontal conical horn antenna with a parabolic reflector at its mouth that re-directed the beam. This particular design had very low sidelobes, and thus made very low receiving system noise temperatures possible. The aperture of the antennas was 3,600 square feet (330 m2). The antennas were 177 feet (54 m) long and weighed 380 short tons (340,000 kg). Morimi Iwama and Jan Norton of Bell Laboratories were in charge of designing and building the electrical portions of the azimuth-elevation system that steered the antennas. The antennas were housed in radomes the size of a 14-story office building. Two of these antennas were used, one in Andover, Maine, and the other in France at Pleumeur-Bodou. The GPO antenna at Goonhilly Downs in Great Britain was a conventional 26-meter-diameter paraboloid.
Telstar 1 relayed its first, and non-public, television pictures--a flag outside Andover Earth Station--to Pleumeur-Bodou on July 11, 1962. Almost two weeks later, on July 23, at 3:00 p.m. EDT, it relayed the first publicly available live transatlantic television signal. The broadcast was shown in Europe by Eurovision and in North America by NBC, CBS, ABC, and the CBC. The first public broadcast featured CBS's Walter Cronkite and NBC's Chet Huntley in New York, and the BBC's Richard Dimbleby in Brussels. The first pictures were the Statue of Liberty in New York and the Eiffel Tower in Paris. The first broadcast was to have been remarks by President John F. Kennedy, but the signal was acquired before the president was ready, so engineers filled the lead-in time with a short segment of a televised game between the Philadelphia Phillies and the Chicago Cubs at Wrigley Field. The batter, Tony Taylor, was seen hitting a ball pitched by Cal Koonce to the right fielder George Altman. From there, the video switched first to Washington, DC; then to Cape Canaveral, Florida; to the Seattle World's Fair; then to Quebec and finally to Stratford, Ontario. The Washington segment included remarks by President Kennedy, talking about the price of the American dollar, which was causing concern in Europe. When Kennedy denied that the United States would devalue the dollar it immediately strengthened on world markets; Cronkite later said that "we all glimpsed something of the true power of the instrument we had wrought."
That evening, Telstar 1 also relayed the first satellite telephone call, between U.S. vice-president Lyndon Johnson and the chairman of AT&T, Frederick Kappel. It successfully transmitted faxes, data, and both live and taped television, including the first live transmission of television across an ocean from Andover, Maine, US, to Goonhilly Downs, England, and Pleumeur-Bodou, France.[clarification needed] (An experimental passive satellite, Echo 1, had been used to reflect and redirect communications signals two years earlier, in 1960.) In August 1962, Telstar 1 became the first satellite used to synchronize time between two continents, bringing the United Kingdom and the United States to within 1 microsecond of each other (previous efforts were only accurate to 2,000 microseconds).
The Telstar 1 satellite also relayed computer data between two IBM 1401 mainframe computers. The test, performed on October 25, 1962, sent a message from a transmitting computer in Endicott, New York, to the earth station in Andover, Maine. The message was relayed to the earth station in France, where it was decoded by a second IBM 1401 in La Gaude, France.
Telstar 1, which had ushered in a new age of the commercial use of technology, became a victim of the military technology of the Cold War era. The day before Telstar 1 launched, a U.S. high-altitude nuclear bomb (called Starfish Prime) had energized the Earth's Van Allen Belt where Telstar 1 went into orbit. This vast increase in a radiation belt, combined with subsequent high-altitude blasts, including a Soviet test in October, overwhelmed Telstar's fragile transistors. It went out of service in November 1962, after handling over 400 telephone, telegraph, facsimile and television transmissions. It was restarted by a workaround in early January 1963.[page needed] The additional radiation associated with its return to full sunlight[clarification needed] once again caused a transistor failure, this time irreparably, and Telstar 1 went out of service on February 21, 1963.
Experiments continued, and by 1964, two Telstars, two Relay units (from RCA), and two Syncom units (from the Hughes Aircraft Company) had operated successfully in space. Syncom 2 was the first geosynchronous satellite and its successor, Syncom 3, broadcast pictures from the 1964 Summer Olympics in Tokyo. The first commercial geosynchronous satellite was Intelsat I ("Early Bird") launched in 1965.
Subsequent Telstar satellites were advanced commercial geosynchronous spacecraft that share only their name with Telstar 1 and 2.
The second wave of Telstar satellites launched with Telstar 301 in 1983, followed by Telstar 302 in 1984 (which was renamed Telstar 3C after it was carried into space by Shuttle mission STS-41-D), and by Telstar 303 in 1985.
The next wave, starting with Telstar 401, came in 1993; which was lost in 1997 due to a magnetic storm, and then Telstar 402 was destroyed shortly after launch in 1994. It was replaced in 1995 by Telstar 402R, eventually renamed Telstar 4.
Telstar 10 was launched in China in 1997 by APT Satellite Company, Ltd.
In 2003, Telstars 4-8 and 13--Loral Skynet's North American fleet--were sold to Intelsat. Telstar 4 suffered complete failure prior to the handover. The others were renamed the Intelsat Americas 5, 6, etc. At the time of the sale, Telstar 8 was still under construction by Space Systems/Loral, and it was finally launched on June 23, 2005, by Sea Launch.
Telstar 18 was launched in June 2004 by sea launch. The upper stage of the rocket underperformed, but the satellite used its significant stationkeeping fuel margin to achieve its operational geostationary orbit. It has enough on-board fuel remaining to allow it to exceed its specified 13-year design life.
|Name||Manufacturer||Launch date||Launch vehicle||Launch place||Orbital position||Bus||Mass|
|Telstar 1||Bell Laboratories||July 10, 1962||Delta-DM19||Cape Canaveral LC-17B||N/A||Telstar Bus||77 kg (170 lb)|
|Telstar 2||Bell Laboratories||May 7, 1963||Delta B||Cape Canaveral LC-17B||N/A||Telstar Bus||79 kg (174 lb)|
|Telstar 301||Hughes||July 28, 1983||Delta-3920 PAM-D||Cape Canaveral LC-17A||76° W||HS-376||625 kg (1,378 lb)|
|Telstar 302||Hughes||August 30, 1984||Discovery||Kennedy LC-39A||125° W||HS-376||625 kg (1,378 lb)|
|Telstar 303||Hughes||June 17, 1985||Discovery||Kennedy LC-39A||76° W||HS-376||630 kg (1,390 lb)|
|Telstar 401||Lockheed Martin||December 16, 1993||Atlas IIAS AC-108||Cape Canaveral LC-36B||97° W||AS-7000||3,375 kg (7,441 lb)|
|Telstar 402||Lockheed Martin||September 9, 1994||Ariane 42L||Kourou ELA-2||89° W
|AS-7000||3,485 kg (7,683 lb)|
|Telstar 4||Lockheed Martin||September 24, 1995||Ariane 42L||Kourou ELA-2||89° W||AS-7000||3,410 kg (7,520 lb)|
|Telstar 5||Space Systems/Loral||May 24, 1997||Proton-K/Block-DM4||Baikonur 81/23||97° W||SSL 1300||3,600 kg (7,900 lb)|
|Telstar 6||Space Systems/Loral||February 15, 1999||Proton-K/Block-DM3||Baikonur 81/23||93° W||SSL 1300||3,763 kg (8,296 lb)|
|Telstar 7||Space Systems/Loral||September 25, 1999||Ariane 44LP||Kourou ELA-2||127° W||SSL 1300||3,790 kg (8,360 lb)|
|Telstar 8||Space Systems/Loral||June 23, 2005||Zenit-3SL||Sea Launch||89° W||SSL 1300S||5,493 kg (12,110 lb)|
|Space Systems/Loral||N/A||N/A||N/A||N/A||SSL 1300S||5,493 kilograms (12,110 lb)|
|Telstar 10||Space Systems/Loral||October 16, 1997||Long March 3B||Xichang 3B||76,5° E||SSL 1300||3,700 kg (8,200 lb)|
|Telstar 11||Matra Marconi Space||November 29, 1994||Atlas IIA||Cape Canaveral LC-36A||37,5° W||Eurostar-2000||2,361 kg (5,205 lb)|
|Telstar 11N||Space Systems/Loral||February 26, 2009||Zenit-3SLB||Baikonur 45/1||37,5° W||SSL 1300||4,012 kg (8,845 lb)|
|Telstar 12||Space Systems/Loral||October 19, 1999||Ariane 44LP||Kourou ELA-2||15° W||SSL 1300||3,814 kg (8,408 lb)|
|Telstar 12V||EADS Astrium||November 24, 2015||H-IIA-204||Tanegashima YLP-1||15° W||Eurostar-3000||5,000 kg (11,000 lb)|
|Telstar 13||Space Systems/Loral||August 8, 2003||Zenit-3SL||Sea Launch||121° W||SSL 1300||4,737 kg (10,443 lb)|
|Telstar 14||Space Systems/Loral||January 11, 2004||Zenit-3SL||Sea Launch||63° W||SSL 1300||4,694 kg (10,348 lb)|
|Telstar 14R||Space Systems/Loral||May 20, 2011||Proton-M/Briz-M||Baikonur 200/39||63° W||SSL 1300||5,000 kg (11,000 lb)|
|Telstar 18||Space Systems/Loral||January 29, 2004||Zenit-3SL||Sea Launch||138° E||SSL 1300||4,640 kg (10,230 lb)|
|Telstar 18V||Space Systems/Loral||September 10, 2018||Falcon 9 B5||Cape Canaveral SLC-40||138° E||SSL 1300||7,060 kg (15,560 lb)|
|Telstar 19V||Space Systems/Loral||July 22, 2018||Falcon 9 B5||Cape Canaveral SLC-40||63° W||SSL 1300||7,076 kg (15,600 lb)|