Syncom

Last updated

Syncom (for "synchronous communication satellite") started as a 1961 NASA program for active geosynchronous communication satellites, all of which were developed and manufactured by the Space and Communications division of Hughes Aircraft Company (now the Boeing Satellite Development Center). Syncom 2, launched in 1963, was the world's first geosynchronous communications satellite. Syncom 3, launched in 1964, was the world's first geostationary satellite. [1]

Contents

In the 1980s, the series was continued as Syncom IV with some much larger satellites, also manufactured by Hughes. They were leased to the United States military under the Leasat program.

Syncom 1, 2 and 3

First generation Syncom satellite Syncom 2 side.jpg
First generation Syncom satellite

Common features

The three early Syncom satellites were experimental spacecraft built by Hughes Aircraft Company's facility in Culver City, California, by a team led by Harold Rosen, Don Williams, and Thomas Hudspeth. [2] All three satellites were cylindrical in shape, with a diameter of about 71 centimeters (28 in) and a height of about 39 centimeters (15 in). Pre-launch fueled masses were 68 kilograms (150 lb), and orbital masses were 39 kilograms (86 lb) with a 25-kilogram (55 lb) payload. They were capable of emitting signals on two transponders at just 2  W. Thus, Syncom satellites were only capable of carrying a single two-way telephone conversation, or 16 Teletype connections. As of 25 June 2009, all three satellites are still in orbit, although no longer functioning. [3]

Syncom 1

Syncom 1 was intended to be the first geosynchronous communications satellite. It was launched on February 14, 1963 with the Delta B #16 launch vehicle from Cape Canaveral, but was lost on the way to geosynchronous orbit due to an electronics failure. [4] Seconds after the apogee kick motor for circularizing the orbit was fired, the spacecraft fell silent. Later telescopic observations verified the satellite was in an orbit with a period of almost 24 hours at a 33° inclination.

Syncom 2

Syncom 2 was launched by NASA on July 26, 1963 [5] with the Delta B #20 launch vehicle from Cape Canaveral. The satellite successfully kept station at the altitude calculated by Herman Potočnik Noordung in the 1920s.

Prime Minister Balewa (2nd from right) talks to President John F. Kennedy on the first live broadcast via the SYNCOM satellite from USNS Kingsport in Lagos, Nigeria. USNS Kingsport SYNCOM Call Kennedy-Balewa July 1963.png
Prime Minister Balewa (2nd from right) talks to President John F. Kennedy on the first live broadcast via the SYNCOM satellite from USNS Kingsport in Lagos, Nigeria.

During the first year of Syncom 2 operations, NASA conducted voice, teletype, and facsimile tests, [5] as well as 110 public demonstrations to show the capabilities of this satellite and invite feedback. In August 1963, President John F. Kennedy in Washington, D.C., telephoned Nigerian Prime Minister Abubakar Tafawa Balewa aboard USNS Kingsport docked in Lagos Harbor—the first live two-way call between heads of government by satellite. The Kingsport acted as a control station and uplink station. [6] [ circular reference ] [7]

Syncom 2 also relayed a number of test television transmissions from Fort Dix, New Jersey to a ground station in Andover, Maine, beginning on September 29, 1963. Although it was low-quality video with no audio, it was the first successful television transmission through a geosynchronous satellite. [5]

Syncom 3

Syncom 3 was the first geostationary communication satellite, launched on August 19, 1964 with the Delta D #25 launch vehicle from Cape Canaveral. The satellite, in orbit near the International Date Line, had the addition of a wideband channel for television and was used to telecast the 1964 Summer Olympics in Tokyo to the United States. [8] Although Syncom 3 is sometimes credited with the first television program to cross the Pacific Ocean, the Relay 1 satellite first broadcast television from the United States to Japan on November 22, 1963. [9] :1

Transfer to Department of Defense control

By the end of 1964, Syncoms 2 and 3 had completed NASA's R&D experiments. On January 1, 1965, NASA transferred operation of the satellites to the United States Department of Defense (DOD) along with telemetry, command stations, and range and rangefinding equipment. DOD had, in fact, provided the communications ground stations used to relay transmissions via the two Syncoms since their launch. DOD agreed to provide telemetry and ranging data of continuing scientific and engineering interest.

In 1965, Syncom 3 was implemented to support the DOD's communications in Vietnam. [10]

Turned off in 1969, Syncom 3 remains in geosynchronous orbit as of December 2012. [11] In 40 years it has drifted 8 degrees to the west, to longitude 172. [12]

Syncom IV (Leasat)

Syncom IV, Hughes-owned US military Leasat Syncom LEASAT.jpg
Syncom IV, Hughes-owned US military Leasat

The five satellites of the 1980s Leasat (Leased Satellite) program (Leasat F1 through Leasat F5) were alternatively named Syncom IV-1 to Syncom IV-5 and called HS 381 by the manufacturer. [13] These satellites were considerably larger than Syncoms 1 to 3, weighing 1.3 tonnes each (over 7 tonnes with launch fuel). At 4.26 meters (14.0 ft), the satellites were the first to be designed for launch from the Space Shuttle payload bay, [14] and were deployed like a Frisbee. [15] The satellites are 30 rpm spin-stabilized with a despun communications and antenna section. They were made with a solid rocket motor for initial perigee burn and hydrazine propellant for station keeping and spin stabilization. The communications systems offers a wideband UHF channel (500 kHz bandwidth), six relay 25 kHz channels, and five narrowband 5 kHz channels. [16] [17] This is in addition to the fleet broadcast frequency, which is in the military's X-band. The system was used by military customers in the US and later in Australia. Most of the satellites were retired in the 1990s, but one would remain operational until 2015. During the First Gulf War, Leasat would be used for personal communications between Secretary of State James Baker and President George H. W. Bush, [18] but was more typically used by "mobile air, surface, subsurface, and fixed earth stations of the Navy, Marine Corps, Air Force, and Army." [16]

Hughes was contracted to provide a worldwide communications system based on four satellites, one over the continental United States (CONUS), and one each over the Atlantic, Pacific, and Indian oceans, spaced about 90 degrees apart. [14] Five satellites were ordered, with one as a replacement. Also part of the contract were the associated control systems and ground stations. The lease contracts were typically for 5-year terms, with the lessee having the opportunity to extend the lease or to purchase the equipment outright. The US Navy was the original lessee.

Leasat F1's launch was cancelled just prior to lift-off, and F2 became the first into orbit on August 30, 1984 aboard Discovery on shuttle mission STS-41-D. F2 was largely successful, but its wideband receiver was out of commission after only 4 months. [18] F1 was launched successfully on November 8, 1984 aboard STS-51-A. This was followed on April 12, 1985 by Leasat F3 on STS-51-D. F3's launch was declared a failure when the satellite failed to start its maneuver to geostationary orbit once released from Discovery. Attempts by Shuttle astronauts to activate F3 with a makeshift "flyswatter" were unsuccessful. [18] The satellite was left in low Earth orbit, and the Space Shuttle returned to Earth. This failure made front-page news in The New York Times . [19] Hughes had an insurance policy on the satellite, and so claimed a total loss for the spacecraft of about $200 million, an amount underwritten by numerous parties.

However, with another satellite planned to be launched, it was determined that a space walk by a subsequent Shuttle crew might be able to "wake" the craft. The best guess was that a switch had failed to turn on the satellite. A "bypass box" was hastily constructed, NASA was excited to offer assistance, the customer was supportive, and the insurance underwriters agreed to fund the attempt at space salvage – a first. [19]

On August 27, 1985 Discovery was again used to launch Leasat F4, and during the same mission (STS-51-I) captured the 15,000 lb stricken F3. Astronaut James van Hoften grappled and then manually spun down the F3 satellite. After the bypass box was installed by van Hoften and Bill Fisher, [20] van Hoften manually spun the satellite up. Once released, the F3 successfully powered up, fired its perigee motor and obtained a geostationary orbit. (This scenario would play out again in 1992 with Intelsat 603 and Endeavour .) While F3 was now operational, Leasat F4 soon failed and was itself declared a loss after only 40 hours of RF communications. [18] [20]

The stricken F4 did not remain a complete failure. Data from F4's failure permitted the saving of F1 from a premature failure. Since all of the Leasats are spin-stabilized, they have a bearing point that connects the non-rotating and rotating parts of the spacecraft. After F4's communication failure, it suffered a spin lock while attempting to jostle the communications payload: the spun and despun sections locked together. [18] Remembering this second failure of F4, and with F1 beginning to wear out at the spin bearing, it was decided to "flip" F1 every six months to keep the payload in the sun. [18] Thus F1 went on to operate smoothly for its remaining life and never encountered a locked despun section.

Leasat F4 was subsequently powered down and moved to a graveyard orbit with a large amount of station keeping fuel in reserve. This was fortuitous; when another satellite suffered a loss of its fuel ten years later, Hughes engineers pioneered the use of alternative propellants with Leasat F4. Long after its primary mission had failed, F4 was powered back on to test whether a satellite could be kept on station using nonvolatile propellants. [18] F4 was used to perform numerous tests, including maneuvers with oxidizer for propulsion once the hydrazine ran out.

The fifth and last Leasat (F5), which was built as a spare, was successfully launched by Columbia mission STS-32 on January 9, 1990. The last active Leasat, it was officially decommissioned on September 24, 2015, at 18:25:13 UTC. [21] F5 was one of the longest-serving and most successful commercial satellites. Towards the end of its 25-year life, F5 had been leased by the Australian Defence Force for UHF service.

DateName ID Launch vehicle
1963-02-14Syncom 1 1963-004A Thor Delta B
1963-07-26Syncom 2 1963-031A Thor Delta B
1964-08-19Syncom 3 1964-047A Thor Delta D
1984-11-10Leasat F1 1984-093C Discovery , STS-51-A
1984-08-31Leasat F2 1984-113C Discovery , STS-41-D
1985-04-12Leasat F3 1985-028C Discovery , STS-51-D
1985-08-29Leasat F4 1985-076D Discovery , STS-51-I
1990-01-09Leasat F5 1990-002B Columbia , STS-32

See also

Related Research Articles

<span class="mw-page-title-main">Geosynchronous orbit</span> Orbit keeping the satellite at a fixed longitude above the equator

A geosynchronous orbit is an Earth-centered orbit with an orbital period that matches Earth's rotation on its axis, 23 hours, 56 minutes, and 4 seconds. The synchronization of rotation and orbital period means that, for an observer on Earth's surface, an object in geosynchronous orbit returns to exactly the same position in the sky after a period of one sidereal day. Over the course of a day, the object's position in the sky may remain still or trace out a path, typically in a figure-8 form, whose precise characteristics depend on the orbit's inclination and eccentricity. A circular geosynchronous orbit has a constant altitude of 35,786 km (22,236 mi).

<span class="mw-page-title-main">Geostationary orbit</span> Circular orbit above Earths Equator and following the direction of Earths rotation

A geostationary orbit, also referred to as a geosynchronous equatorial orbit (GEO), is a circular geosynchronous orbit 35,786 km (22,236 mi) in altitude above Earth's equator, 42,164 km (26,199 mi) in radius from Earth's center, and following the direction of Earth's rotation.

<span class="mw-page-title-main">Communications satellite</span> Artificial satellite that relays radio signals

A communications satellite is an artificial satellite that relays and amplifies radio telecommunication signals via a transponder; it creates a communication channel between a source transmitter and a receiver at different locations on Earth. Communications satellites are used for television, telephone, radio, internet, and military applications. Many communications satellites are in geostationary orbit 22,300 miles (35,900 km) above the equator, so that the satellite appears stationary at the same point in the sky; therefore the satellite dish antennas of ground stations can be aimed permanently at that spot and do not have to move to track the satellite. Others form satellite constellations in low Earth orbit, where antennas on the ground have to follow the position of the satellites and switch between satellites frequently.

<span class="mw-page-title-main">STS-32</span> 1990 American crewed spaceflight to retrieve the Long Duration Exposure Facility

STS-32 was the 33rd mission of NASA's Space Shuttle program, and the ninth launch of Space ShuttleColumbia. Launched on January 9, 1990, it marked the first use of the Launch Complex 39A of Kennedy Space Center at since 1986; it also marked the first use of Mobile Launcher Platform-3 (MLP-3) in the Space Shuttle program. STS-32 was, at the time, the longest shuttle mission yet conducted, with a duration of nearly 11 days. Before STS-32, the only mission of the same duration had been STS-9 in 1983. On January 20, 1990, STS-32 executed the third night landing of the shuttle program. STS-32 was also the first Shuttle mission of the 1990s.

<span class="mw-page-title-main">STS-41-D</span> 1984 American crewed spaceflight and maiden flight of Space Shuttle Discovery

STS-41-D was the 12th flight of NASA's Space Shuttle program, and the first mission of Space Shuttle Discovery. It was launched from Kennedy Space Center, Florida, on August 30, 1984, and landed at Edwards Air Force Base, California, on September 5, 1984. Three commercial communications satellites were deployed into orbit during the six-day mission, and a number of scientific experiments were conducted, including a prototype extendable solar array that would eventually form the basis of the main solar arrays on the International Space Station (ISS).

<span class="mw-page-title-main">STS-51-I</span> 1985 American crewed spaceflight to Syncom IV-3

STS-51-I was the 20th mission of NASA's Space Shuttle program and the sixth flight of Space Shuttle Discovery. During the mission, Discovery deployed three communications satellites into orbit. The mission launched from Kennedy Space Center, Florida, on August 27, 1985, and landed at Edwards Air Force Base, California, on September 3, 1985.

<span class="mw-page-title-main">STS-49</span> 1992 American crewed spaceflight to Intelsat 603 and maiden flight of Shuttle Endeavour

STS-49 was NASA's maiden flight of the Space Shuttle Endeavour, which launched on May 7, 1992. The primary goal of its nine-day mission was to retrieve an Intelsat VI satellite, Intelsat 603, which failed to leave Low Earth orbit two years before, attach it to a new upper stage, and relaunch it to its intended geosynchronous orbit. After several attempts, the capture was completed with the only three-person extravehicular activity (EVA) in space flight history. It would also stand until STS-102 in 2001 as the longest EVA ever undertaken.

The Boeing Satellite Development Center is a major business unit of Boeing Defense, Space & Security. It brought together Boeing satellite operations with that of GM Hughes Electronics' Space and Communications division in El Segundo, California.

<span class="mw-page-title-main">SBS 4</span>

SBS 4 was a geostationary communications satellite designed and manufactured by Hughes on the HS-376 platform. It was ordered by Satellite Business Systems, which later sold it to Hughes Communications. It had a Ku band payload and operated at 94°W longitude.

<span class="mw-page-title-main">Intelsat I</span> American commercial communications satellite launched in 1965

Intelsat I was the first commercial communications satellite to be placed in geosynchronous orbit, on April 6, 1965. It was built by the Space and Communications Group of Hughes Aircraft Company for COMSAT, which activated it on June 28, 1965. It was based on the Syncom series of satellites that Hughes had previously built for NASA to demonstrate that communications via synchronous-orbit satellite were feasible. Its booster was a Thrust Augmented Delta. After a series of maneuvers, it reached its geosynchronous orbital position over the Atlantic Ocean at 28° West longitude, where it was put into service.

<span class="mw-page-title-main">Tracking and data relay satellite</span> American communications satellite

A tracking and data relay satellite (TDRS) is a type of communications satellite that forms part of the Tracking and Data Relay Satellite System (TDRSS) used by NASA and other United States government agencies for communications to and from independent "User Platforms" such as satellites, balloons, aircraft, the International Space Station, and remote bases like the Amundsen-Scott South Pole Station. This system was designed to replace an existing worldwide network of ground stations that had supported all of NASA's crewed flight missions and uncrewed satellites in low-Earth orbits. The primary system design goal was to increase the amount of time that these spacecraft were in communication with the ground and improve the amount of data that could be transferred. These TDRSS satellites are all designed and built to be launched to and function in geosynchronous orbit, 35,786 km (22,236 mi) above the surface of the Earth.

<span class="mw-page-title-main">Morelos Satellite System</span> Series of Mexican communications satellites

The Morelos satellites are a series of Mexican communications satellites. The first two operated between 1985 and 1998 and provided telephony, data, and television services over the territory of the Mexican Republic and adjacent areas. The third is now part of the MEXSAT constellation but carries the Morelos name.

Marisat satellites were the first maritime telecommunications satellites and were designed to provide dependable telecommunications for commercial shipping and the U.S. Navy from stable geosynchronous orbital locations over the three major ocean regions. The three Marisat satellites, F1, F2, and F3, were built by Hughes Aircraft Corporation (HAC) for COMSAT Corporation starting in 1973. The satellites were designed to provide maritime telecommunications services in three large ocean areas, the Atlantic Ocean, the Pacific Ocean, and the Indian Ocean, and were located at 72.5° East longitude, 176.5° E, and 345° E in the geosynchronous orbital arc. The three-satellite Marisat system served as the initial INMARSAT constellation.

<span class="mw-page-title-main">TDRS-5</span> American communications satellite

TDRS-5, known before launch as TDRS-E, 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 is based on a custom satellite bus which was used for all seven first generation TDRS satellites.

Orion 3 was an American spacecraft which was intended for use by Orion Network Systems, as a geostationary communications satellite. It was to have been positioned in geostationary orbit at a longitude of 139° East, from where it was to have provided communications services to Asia and Oceania. Due to a malfunction during launch, it was instead delivered to a useless low Earth orbit.

<span class="mw-page-title-main">TDRS-3</span> American communications satellite

TDRS-3, known before launch as TDRS-C, 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, and is based on a custom satellite bus which was used for all seven first generation TDRS satellites.

<span class="mw-page-title-main">TDRS-6</span> American communications satellite

TDRS-6, known before launch as TDRS-F, 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, and is based on a custom satellite bus which was used for all seven first generation TDRS satellites.

<span class="mw-page-title-main">Telstar</span> Name of various communications satellites

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 was launched May 7, 1963. Telstar 1 and 2—though no longer functional—still orbit the Earth.

On-orbit satellite servicing refers to refueling or repairing space satellites while in orbit.

<span class="mw-page-title-main">SBS 3 (satellite)</span> Satellite Launched on STS-5

SBS 3 was a geostationary communications satellite designed and manufactured by Hughes on the HS-376 platform. It was ordered by Satellite Business Systems, which later sold it to Hughes Communications. It had a Ku band payload and operated on the 94°W longitude.

References

  1. "Syncom 1, 2, 3". Gunter's Space Page. Retrieved March 10, 2013. Syncom 3 was the first geostationary satellite...It was...placed over the equator at 180 degrees longitude in the Pacific Ocean. The satellite provided live television coverage of the 1964 Olympic games in Tokyo, Japan...
  2. Zach Wichter (February 2, 2017). "Harold Rosen, Who Ushered in the Era of Communication Satellites, Dies at 90". The New York Times.
  3. "U.S. Space Objects Registry". Archived from the original on October 6, 2013. Retrieved June 25, 2009.
  4. "The Room-Size World". TIME . May 14, 1965. Archived from the original on May 20, 2009.
  5. 1 2 3 Henry, Varice F.; McDonald, Michael E. (July 1965). "Television Tests with the Syncom II Synchronous Communications Satellite (NASA technical note D-2911)" (PDF). NTRS.nasa.gov. NASA. Archived (PDF) from the original on October 9, 2022. Retrieved December 7, 2014.
  6. Uhlig, Thomas; Sellmaier, Florian; Schmidhuber, Michael (2014). Spacecraft Operations. New York: Springer. ISBN   9783709118023. LCCN   2014945749 . Retrieved June 13, 2020.
  7. Williamson, Mark (2006). Spacecraft Technology: the early years. London: Institution of Electrical Engineers. ISBN   9780863415531. LCCN   2008530215 . Retrieved June 13, 2020.
  8. "For Gold, Silver & Bronze". TIME . October 16, 1964. Archived from the original on April 21, 2008.
  9. "Significant Achievements in Space Communications and Navigation, 1958-1964" (PDF). NASA-SP-93. NASA. 1966. pp. 30–32. Archived (PDF) from the original on October 9, 2022. Retrieved October 31, 2009.
  10. "Aeronautics and Astronautics, 1965" (PDF). NASA. 1966. Archived (PDF) from the original on October 9, 2022. Retrieved January 2, 2019.
  11. "Detailed information about SYNCOM 3 satellite, 1964-047A, TLE data for Norad 858". Satellite Tracking, Prediction and Informations about Objects in the Sky. Infosatellites.com. Archived from the original on March 4, 2016. The spacecraft next carried out a series of attitude and velocity maneuvers to align itself with the equator at an inclination of 0.1 degrees and to slow its speed so it drifted west to the planned location at 180 degrees longitude where its speed at altitude was synchronized with the Earth.
  12. "Track SYNCOM 3 Satellite in Real Time". Satellite Tracking, Prediction and Informations about Objects in the Sky. Infosatellites.com. Archived from the original on March 4, 2016. Requires Javascript.
  13. "The Men Who Staff HCI's LEASAT Earth Stations Are Accustomed To Working On Their Own". Uplink. Hughes Communications. Summer 1994. Archived from the original on May 5, 1999.
  14. 1 2 "LEASAT". Military Space Programs. Federation of American Scientists. Archived from the original on June 23, 2012.
  15. Jack Fisher (January 3, 2013). "Leasat Beginnings and Significance–Boris Subbotin". Our Space Heritage 1960-2000.
  16. 1 2 "First Satellite Designed for Space Shuttle Launch". Defense, Space & Security. Boeing. Archived from the original on December 30, 2009.
  17. "Leasat 1, 2, 3, 4, 5 (Syncom-4 1, 2, 3, 4, 5)". Gunter's Space Page. Retrieved January 2, 2020.
  18. 1 2 3 4 5 6 7 Jack Fisher (November 2, 2015). "LEASAT F5, The Final Chapter-Andy Ott". Our Space Heritage 1960-2000.
  19. 1 2 Jack Fisher (April 23, 2013). "The Leasat Rescue Mission—Steve Dorfman". Our Space Heritage 1960-2000.
  20. 1 2 "The LEASAT Program That Launched HCI Completes 13 Years Of Service". Uplink. Hughes Communications. Winter 1993. Archived from the original on May 7, 1999.
  21. Nerenberg, Sharyn (January 24, 2015). "Another Intelsat Satellite Serves Customers for More Than 25 Years". Intelsat. Archived from the original on September 26, 2015. Retrieved September 25, 2015.

Further reading