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NASA Deep Space Network

The NASA Deep Space Network (DSN) is a worldwide network of spacecraft communication ground segment facilities, located in the United States (California), Spain (Madrid), and Australia (Canberra), that supports NASA's interplanetary spacecraft missions. It also performs radio and radar astronomy observations for the exploration of the Solar System and the universe, and supports selected Earth-orbiting missions. DSN is part of the NASA Jet Propulsion Laboratory (JPL).

Deep Space Network
Insignia for the Deep Space Network's 50th anniversary celebrations (1963–2013)
Alternative namesNASA Deep Space Network
OrganizationInterplanetary Network Directorate
(NASA / JPL)
LocationPasadena, Los Angeles County, California, Pacific States Region
Coordinates34°12′6.1″N 118°10′18″W / 34.201694°N 118.17167°W / 34.201694; -118.17167
EstablishedOctober 1, 1958 (1958-10-01)
65 years ago
Websitedeepspace.jpl.nasa.gov
Telescopes
  Related media on Commons

General information edit

 
Deep Space Network Operations Center at JPL, Pasadena (California) in 1993.

DSN currently consists of three deep-space communications facilities located such that a distant spacecraft is always in view of at least one station.[1][2][3] They are:

Each facility is situated in semi-mountainous, bowl-shaped terrain to help shield against radio frequency interference.[4] The strategic placement of the stations permits constant observation of spacecraft as the Earth rotates, which helps to make the DSN the largest and most sensitive scientific telecommunications system in the world.[5]

The DSN supports NASA's contribution to the scientific investigation of the Solar System: It provides a two-way communications link that guides and controls various NASA uncrewed interplanetary space probes, and brings back the images and new scientific information these probes collect. All DSN antennas are steerable, high-gain, parabolic reflector antennas.[4] The antennas and data delivery systems make it possible to:[2]

  • acquire telemetry data from spacecraft.
  • transmit commands to spacecraft.
  • upload software modifications to spacecraft.
  • track spacecraft position and velocity.
  • perform Very Long Baseline Interferometry observations.
  • measure variations in radio waves for radio science experiments.
  • gather science data.
  • monitor and control the performance of the network.

Other countries and organizations also run deep space networks. The DSN operates according to the standards of the Consultative Committee for Space Data Systems, as do most other deep space networks, and hence the DSN is able to inter-operate with the networks of other space agencies. These include the Soviet Deep Space Network, the Chinese Deep Space Network, the Indian Deep Space Network, the Japanese Deep Space Network, and the ESTRACK of the European Space Agency. These agencies often cooperate for better mission coverage.[6] In particular, DSN has a cross-support agreement with ESA that allows mutual use of both networks for more effectiveness and reduced risk.[7] In addition, radio astronomy facilities, such as Parkes Observatory or the Green Bank Telescope, are sometimes used to supplement the antennas of the DSN.

Operations control center edit

The antennas at all three DSN Complexes communicate directly with the Deep Space Operations Center (also known as Deep Space Network operations control center) located at the JPL facilities in Pasadena, California.[3]

In the early years, the operations control center did not have a permanent facility. It was a provisional setup with numerous desks and phones installed in a large room near the computers used to calculate orbits. In July 1961, NASA started the construction of the permanent facility, Space Flight Operations Facility (SFOF). The facility was completed in October 1963 and dedicated on May 14, 1964. In the initial setup of the SFOF, there were 31 consoles, 100 closed-circuit television cameras, and more than 200 television displays to support Ranger 6 to Ranger 9 and Mariner 4.[8]

Currently, the operations center personnel at SFOF monitor and direct operations, and oversee the quality of spacecraft telemetry and navigation data delivered to network users. In addition to the DSN complexes and the operations center, a ground communications facility provides communications that link the three complexes to the operations center at JPL, to space flight control centers in the United States and overseas, and to scientists around the world.[9]

Deep space edit

 
View from the Earth's north pole, showing the field of view of the main DSN antenna locations. Once a mission gets more than 30,000 km (19,000 mi) from Earth, it is al­ways in view of at least one of the stations.

Tracking vehicles in deep space is quite different from tracking missions in low Earth orbit (LEO). Deep space missions are visible for long periods of time from a large portion of the Earth's surface, and so require few stations (the DSN has only three main sites). These few stations, however, require huge antennas, ultra-sensitive receivers, and powerful transmitters in order to transmit and receive over the vast distances involved.

Deep space is defined in several different ways. According to a 1975 NASA report, the DSN was designed to communicate with "spacecraft traveling approximately 16,000 km (10,000 miles) from Earth to the farthest planets of the solar system."[10] JPL diagrams[11] state that at an altitude of 30,000 km (19,000 mi), a spacecraft is always in the field of view of one of the tracking stations.

Frequency bands edit

The International Telecommunication Union, which sets aside various frequency bands for deep space and near Earth use, defines "deep space" to start at a distance of 2 million km (1.2 million mi) from the Earth's surface.[12] These are in S-band, X-band, K-band and Ka-band.

Because the Moon, the Earth-moon Lagrange points, and the Earth–Sun Lagrangian points L1 and L2, are all closer than 2 million km from Earth (distances are here), they are considered near space and cannot use the ITU's deep space bands.

History edit

The forerunner of the DSN was established in January 1958, when JPL, then under contract to the U.S. Army, deployed portable radio tracking stations in Nigeria, Singapore, and California to receive telemetry and plot the orbit of the Army-launched Explorer 1, the first successful U.S. satellite.[13] NASA was officially established on October 1, 1958, to consolidate the separately developing space-exploration programs of the US Army, US Navy, and US Air Force into one civilian organization.[14]

On December 3, 1958, JPL was transferred from the US Army to NASA and given responsibility for the design and execution of lunar and planetary exploration programs using remotely controlled spacecraft. Shortly after the transfer, NASA established the concept of the Deep Space Network as a separately managed and operated communications system that would accommodate all deep space missions, thereby avoiding the need for each flight project to acquire and operate its own specialized space communications network. The DSN was given responsibility for its own research, development, and operation in support of all of its users. Under this concept, it has become a world leader in the development of low-noise receivers; large parabolic-dish antennas; tracking, telemetry, and command systems; digital signal processing; and deep space navigation. The Deep Space Network formally announced its intention to send missions into deep space on Christmas Eve 1963; it has remained in continuous operation in one capacity or another ever since.[15]

The largest antennas of the DSN are often called on during spacecraft emergencies. Almost all spacecraft are designed so normal operation can be conducted on the smaller (and more economical) antennas of the DSN, but during an emergency the use of the largest antennas is crucial. This is because a troubled spacecraft may be forced to use less than its normal transmitter power, attitude control problems may preclude the use of high-gain antennas, and recovering every bit of telemetry is critical to assessing the health of the spacecraft and planning the recovery. The most famous example is the Apollo 13 mission, where limited battery power and inability to use the spacecraft's high-gain antennas reduced signal levels below the capability of the Manned Space Flight Network, and the use of the biggest DSN antennas (and the Australian Parkes Observatory radio telescope) was critical to saving the lives of the astronauts. While Apollo was also a US mission, DSN provides this emergency service to other space agencies as well, in a spirit of inter-agency and international cooperation. For example, the recovery of the Solar and Heliospheric Observatory (SOHO) mission of the European Space Agency (ESA) would not have been possible without the use of the largest DSN facilities.

DSN and the Apollo program edit

Although normally tasked with tracking uncrewed spacecraft, the Deep Space Network (DSN) also contributed to the communication and tracking of Apollo missions to the Moon, although primary responsibility was held by the Manned Space Flight Network (MSFN). The DSN designed the MSFN stations for lunar communication and provided a second antenna at each MSFN site (the MSFN sites were near the DSN sites for just this reason). Two antennas at each site were needed both for redundancy and because the beam widths of the large antennas needed were too small to encompass both the lunar orbiter and the lander at the same time. DSN also supplied some larger antennas as needed, in particular for television broadcasts from the Moon, and emergency communications such as Apollo 13.[16]

Excerpt from a NASA report describing how the DSN and MSFN cooperated for Apollo:[17]

Another critical step in the evolution of the Apollo Network came in 1965 with the advent of the DSN Wing concept. Originally, the participation of DSN 26-m antennas during an Apollo Mission was to be limited to a backup role. This was one reason why the MSFN 26-m sites were collocated with the DSN sites at Goldstone, Madrid, and Canberra. However, the presence of two, well-separated spacecraft during lunar operations stimulated the rethinking of the tracking and communication problem. One thought was to add a dual S-band RF system to each of the three 26-m MSFN antennas, leaving the nearby DSN 26-m antennas still in a backup role. Calculations showed, though, that a 26-m antenna pattern centered on the landed Lunar Module would suffer a 9-to-12 db loss at the lunar horizon, making tracking and data acquisition of the orbiting Command Service Module difficult, perhaps impossible. It made sense to use both the MSFN and DSN antennas simultaneously during the all-important lunar operations. JPL was naturally reluctant to compromise the objectives of its many uncrewed spacecraft by turning three of its DSN stations over to the MSFN for long periods. How could the goals of both Apollo and deep space exploration be achieved without building a third 26-m antenna at each of the three sites or undercutting planetary science missions?

The solution came in early 1965 at a meeting at NASA Headquarters, when Eberhardt Rechtin suggested what is now known as the "wing concept". The wing approach involves constructing a new section or "wing" to the main building at each of the three involved DSN sites. The wing would include a MSFN control room and the necessary interface equipment to accomplish the following:

  1. Permit tracking and two-way data transfer with either spacecraft during lunar operations.
  2. Permit tracking and two-way data transfer with the combined spacecraft during the flight to the Moon.
  3. Provide backup for the collocated MSFN site passive track (spacecraft to ground RF links) of the Apollo spacecraft during trans-lunar and trans-earth phases.

With this arrangement, the DSN station could be quickly switched from a deep-space mission to Apollo and back again. GSFC personnel would operate the MSFN equipment completely independently of DSN personnel. Deep space missions would not be compromised nearly as much as if the entire station's equipment and personnel were turned over to Apollo for several weeks.

The details of this cooperation and operation are available in a two-volume technical report from JPL.[18][19]

Management edit

The network is a NASA facility and is managed and operated for NASA by JPL, which is part of the California Institute of Technology (Caltech). The Interplanetary Network Directorate (IND) manages the program within JPL and is charged with the development and operation of it. The IND is considered to be JPL's focal point for all matters relating to telecommunications, interplanetary navigation, information systems, information technology, computing, software engineering, and other relevant technologies. While the IND is best known for its duties relating to the Deep Space Network, the organization also maintains the JPL Advanced Multi-Mission Operations System (AMMOS) and JPL's Institutional Computing and Information Services (ICIS).[20][21]

The facilities in Spain and Australia are jointly owned and operated in conjunction with that government's scientific institutions. In Australia, "the Commonwealth Scientific and Industrial Research Organisation (CSIRO), an Australian Commonwealth Government Statutory Authority, established the CSIRO Astronomy and Space Science Division to manage the day-to-day operations, engineering, and maintenance activities of the Canberra Deep Space Communications Complex".[22] Most of the staff at Tidbinbilla are Australian government employees; the land and buildings are owned by the Australian government; NASA provides the bulk of the funding, owns the movable property (such as dishes and electronic equipment) which it has paid for, and gets to decide where to point the dishes.[23] Similarly, in Spain, "Ingenieria de Sistemas para la Defensa de España S.A. (ISDEFE), a wholly owned subsidiary of the Instituto Nacional de Técnica Aeroespacial (INTA) and a part of the Spanish Department of Defense, operates and maintains the Madrid Deep Space Communications Complex (Madrid)".[22]

Peraton (formerly Harris Corporation) is under contract to JPL for the DSN's operations and maintenance. Peraton has responsibility for managing the Goldstone complex, operating the DSOC, and for DSN operations, mission planning, operations engineering, and logistics.[24][25][26]

Antennas edit

 
70 m antenna at Goldstone, California.

Each complex consists of at least four deep space terminals equipped with ultra-sensitive receiving systems and large parabolic-dish antennas. There are:

Five of the 34-meter (112 ft) beam waveguide antennas were added to the system in the late 1990s. Three were located at Goldstone, and one each at Canberra and Madrid. A second 34-meter (112 ft) beam waveguide antenna (the network's sixth) was completed at the Madrid complex in 2004.

In order to meet the current and future needs of deep space communication services, a number of new Deep Space Station antennas had to be built at the existing Deep Space Network sites. At the Canberra Deep Space Communication Complex the first of these was completed in October 2014 (DSS35), with a second becoming operational in October 2016 (DSS36).[27] A new 34 meter dish (DSS53) became operational at the Madrid complex in February 2022.[28]

By 2025, the 70-meter antennas at all three locations will be decommissioned and replaced with 34-meter BWG antennas that will be arrayed. All systems will be upgraded to have X-band uplink capabilities and both X and Ka-band downlink capabilities.[29]

Current signal processing capabilities edit

 
The Canberra Deep Space Communication Complex in 2008

The general capabilities of the DSN have not substantially changed since the beginning of the Voyager Interstellar Mission in the early 1990s. However, many advancements in digital signal processing, arraying and error correction have been adopted by the DSN.

The ability to array several antennas was incorporated to improve the data returned from the Voyager 2 Neptune encounter, and extensively used for the Galileo mission, when the spacecraft's high-gain antenna failed to deploy and as a result Galileo was forced to resort to operating solely off its low-gain antennas.[30]

The DSN array currently available since the Galileo mission can link the 70-meter (230 ft) dish antenna at the Deep Space Network complex in Goldstone, California, with an identical antenna located in Australia, in addition to two 34-meter (112 ft) antennas at the Canberra complex. The California and Australia sites were used concurrently to pick up communications with Galileo.

Arraying of antennas within the three DSN locations is also used. For example, a 70-meter (230 ft) dish antenna can be arrayed with a 34-meter dish. For especially vital missions, like Voyager 2, non-DSN facilities normally used for radio astronomy can be added to the array.[31] In particular, the Canberra 70-meter (230 ft) dish can be arrayed with the Parkes Radio Telescope in Australia; and the Goldstone 70-meter dish can be arrayed with the Very Large Array of antennas in New Mexico.[32] Also, two or more 34-meter (112 ft) dishes at one DSN location are commonly arrayed together.

All the stations are remotely operated from a centralized Signal Processing Center at each complex. These Centers house the electronic subsystems that point and control the antennas, receive and process the telemetry data, transmit commands, and generate the spacecraft navigation data. Once the data are processed at the complexes, they are transmitted to JPL for further processing and for distribution to science teams over a modern communications network.

Especially at Mars, there are often many spacecraft within the beam width of an antenna. For operational efficiency, a single antenna can receive signals from multiple spacecraft at the same time. This capability is called Multiple Spacecraft Per Aperture, or MSPA. Currently, the DSN can receive up to 4 spacecraft signals at the same time, or MSPA-4. However, apertures cannot currently be shared for uplink. When two or more high-power carriers are used simultaneously, very high order intermodulation products fall in the receiver bands, causing interference to the much (25 orders of magnitude) weaker received signals.[33] Therefore, only one spacecraft at a time can get an uplink, though up to 4 can be received.

Network limitations and challenges edit

 
70m antenna in Robledo de Chavela, Community of Madrid, Spain

There are a number of limitations to the current DSN, and a number of challenges going forward.

  • The Deep Space Network nodes are all on Earth. Therefore, data transmission rates from/to spacecraft and space probes are severely constrained due to the distances from Earth. For now it can connect with the Mars orbiters in the Mars Relay Network for faster and more flexible communications with spacecraft and landers on Mars.[34] Adding dedicated communication satellites elsewhere in space, to handle multiparty, multi-mission use, such as the canceled Mars Telecommunications Orbiter, would increase flexibility towards some sort of Interplanetary Internet.
  • The need to support "legacy" missions that have remained operational beyond their original lifetimes but are still returning scientific data. Programs such as Voyager have been operating long past their original mission termination date. They also need some of the largest antennas.
  • Replacing major components can cause problems as it can leave an antenna out of service for months at a time.
  • The older 70 m antennas are reaching the end of their lives. At some point these will need to be replaced. The leading candidate for 70 m replacement had been an array of smaller dishes,[35][36] but more recently the decision was taken to expand the provision of 34-meter (112 ft) BWG antennas at each complex to a total of 4.[37] All the 34-meter HEF antennas have been replaced.
  • New spacecraft intended for missions beyond geocentric orbits are being equipped to use the beacon mode service, which allows such missions to operate without the DSN most of the time.[38]

DSN and radio science edit

 
Illustration of Juno and Jupiter. Juno is in a polar orbit that takes it close to Jupiter as it passes from north to south, getting a view of both poles. During the GS experiment it must point its antenna at the Deep Space Network on Earth to pick up a special signal sent from DSN.

The DSN forms one portion of the radio sciences experiment included on most deep space missions, where radio links between spacecraft and Earth are used to investigate planetary science, space physics and fundamental physics. The experiments include radio occultations, gravity field determination and celestial mechanics, bistatic scattering, doppler wind experiments, solar corona characterization, and tests of fundamental physics.[39]

For example, the Deep Space Network forms one component of the gravity science experiment on Juno. This includes special communication hardware on Juno and uses its communication system.[40] The DSN radiates a Ka-band uplink, which is picked up by Juno's Ka-Band communication system and then processed by a special communication box called KaTS, and then this new signal is sent back the DSN.[40] This allows the velocity of the spacecraft over time to be determined with a level of precision that allows a more accurate determination of the gravity field at planet Jupiter.[40][41]

Another radio science experiment is REX on the New Horizons spacecraft to Pluto-Charon. REX received a signal from Earth as it was occulted by Pluto, to take various measurements of that system of bodies.

See also edit

References edit

  1. ^ Haynes, Robert (1987). How We Get Pictures From Space (PDF). NASA Facts (Revised ed.). NASA. (PDF) from the original on April 18, 2022. Retrieved September 19, 2013.
  2. ^ a b . JPL. Archived from the original on 2012-06-08. Retrieved 2012-06-08.
  3. ^ a b Latifiyan, Pouya (April 2021). "Space Telecommunications, how?". Take off. 1. Tehran: Civil Aviation Technology College: 15 – via Persian.
  4. ^ a b . JPL, NASA. Archived from the original on 2011-04-11.
  5. ^ . science.nasa.gov. NASA. Archived from the original on May 15, 2017. Retrieved May 17, 2018.
  6. ^ Susan Kurtik (23 April 2013). "Deep Space Network (DSN) Mission Services and Operations Interface for Small Deep Space Missions" (PDF). Jet Propulsion Laboratory. hdl:2014/44347. S2CID 117882864. (PDF) from the original on 2022-04-18.
  7. ^ Warhaut, Manfred; Braukus, Michael (April 2, 2007). "ESA and NASA extend ties with major new cross-support agreement". www.esa.int (Press release). ESA. from the original on February 5, 2023. Retrieved July 5, 2020.
  8. ^ . Picture Album of the DEEP SPACE NETWORK. NASA/JPL. Archived from the original on 17 February 2013. Retrieved 26 January 2014.
  9. ^ (PDF). JPL. Archived from the original (PDF) on 2020-04-26. Retrieved 2011-03-25.
  10. ^ Renzetti, N. (May 1975). DSN Functions and Facilities (PDF) (Technical report). JPL. (PDF) from the original on September 3, 2023.
  11. ^ Deutsch, Les (June 24, 2012). NASA's Deep Space Network: Big Antennas with a Big Job. Anten Sympoisum, Toulouse Space Show (PDF). Toulouse, France: JPL. p. 25. hdl:2014/42668. from the original on January 21, 2024.
  12. ^ (PDF). December 15, 2009. Archived from the original (PDF) on June 11, 2014. Retrieved July 13, 2014.
  13. ^ Mudgway, Douglas J. (2001). Uplink-Downlink: A History of the Deep Space Network, 1957–1997 (PDF). p. 5. SP-2001-4227. (PDF) from the original on April 11, 2023.
  14. ^ NASA (2005). "The National Aeronautics and Space Act". NASA. Retrieved November 9, 2007.
  15. ^ Stirone, Shannon (March 2018). "Welcome to the Center of the Universe". LongReads. from the original on December 2, 2023. Retrieved March 17, 2018.
  16. ^ Soumyajit Mandal. (PDF). Archived from the original (PDF) on July 20, 2011. Retrieved July 2, 2008.
  17. ^ William R. Corliss (June 1974). NASA Technical report CR 140390, Histories of the Space Tracking and Data Acquisition Network (STADAN), the Manned Space Flight Network (MSFN), and the NASA Communications Network (NASCOM) (PDF) (Report). NASA. hdl:2060/19750002909. (PDF) from the original on 2022-03-03. 100MB PDF file. Explicitly non-copyrighted.
  18. ^ Flanagan, F. M.; Goodwin, P. S.; Renzetti, N. A. (July 15, 1970). Deep Space Network Support of the Manned Space Flight Network for Apollo, 1962–1968 (PDF) (Technical report). Vol. 1. NASA. JPL-TM-33-452-VOL-1/NASA-CR-116801. (PDF) from the original on May 21, 2022.
  19. ^ Flanagan, F. M.; Goodwin, P. S.; Renzetti, N. A. (May 1971). Deep Space Network Support of the Manned Space Flight Network for Apollo, 1969–1970 (PDF) (Technical report). Vol. 2. NASA. JPL-TM-33-452-VOL-2/NASA-CR-118325. (PDF) from the original on April 18, 2022.
  20. ^ . JPL. Archived from the original on 2009-04-11.
  21. ^ Weber, William J. (May 27, 2004). Interplanetary Network Directorate. 7th Briefing for Industry (PDF). Pasadena, California: JPL. hdl:2014/40704. from the original on January 21, 2024.
  22. ^ a b "NASA'S MANAGEMENT OF THE DEEP SPACE NETWORK" (PDF).
  23. ^ "Agreement between the Government of Australia and the Government of the United States of America for Space Vehicle Tracking and Communication Facilities".
  24. ^ Lackey, Leah (May 23, 2013). "ITT Exelis selected for NASA Deep Space Network subcontract by Jet Propulsion Laboratory" (Press release). ITT Exelis. Archived from the original on January 21, 2024. Retrieved July 5, 2016 – via SpaceRef.
  25. ^ Gelles, David (February 6, 2015). "Harris Corporation to Buy Defense Contractor Exelis for $4.7 Billion". DealBook. The New York Times. from the original on March 26, 2023. Retrieved October 31, 2016.
  26. ^ "CONTRACT to PERATON INC". USAspending. Retrieved 2023-05-15.
  27. ^ "Antennas". NASA. from the original on June 6, 2023. Retrieved July 13, 2015.
  28. ^ O'Neill, Ian J.; Pamer, Melissa. "NASA Adds Giant New Dish to Communicate with Deep Space Network" (Press release). JPL. from the original on January 17, 2024. Retrieved November 17, 2022.
  29. ^ . nasa.gov. May 16, 2018. Archived from the original on February 5, 2015. Retrieved May 16, 2018.
  30. ^ Uplink-Downlink, Chapter 5, The Galileo Era – 1986–1996.
  31. ^ Brown, D. W.; Brundage, W. D.; Ulvestad, J. S.; Kent, S. S.; Bartos, K. P. (August 15, 1990). Interagency Telemetry Arraying for the Voyager-Neptune Encounter (PDF) (Technical report). JPL. TDA Progress Report 42-102. (PDF) from the original on November 17, 2023.
  32. ^ "Antenna Arraying". JPL. 30 March 2020.
  33. ^ Conroy, B. L.; Hoppe, D. J. (November 15, 1996). Noise Bursts and Intermodulation Products Caused by Multiple Carriers at X-Band (PDF) (Technical report). JPL. TDA Progress Report 42-127. (PDF) from the original on December 6, 2023.
  34. ^ O’Neill, Ian J.; Hautaluoma, Grey; Johnson, Alana (February 16, 2021). "The Mars Relay Network Connects Us to NASA's Martian Explorers". NASA’s Mars Exploration Program (Press release). NASA. from the original on January 11, 2024. Retrieved March 10, 2021.
  35. ^ . JPL. Archived from the original on July 14, 2009.
  36. ^ Durgadas S. Bagri; Joseph I. Statman & Mark S. Gatti (2007). "Proposed Array-Based Deep Space Network for NASA". Proceedings of the IEEE. 95 (10). IEEE: 1916–1922. doi:10.1109/JPROC.2007.905046. S2CID 27224753.
  37. ^ "DSN Aperature Enhancement Project". NASA. November 10, 2012. from the original on February 5, 2015. Retrieved June 6, 2013.
  38. ^ Wyatt, E. Jay; Foster, Mike; Schlutsmeyer, Alan; Sherwood, Rob; Sue, Miles K. An Overview of the Beacon Monitor Operations Technology (PDF) (Technical report). JPL. (PDF) from the original on March 21, 2023.
  39. ^ . JPL. Archived from the original on 2016-12-03.
  40. ^ a b c "European Involvement in Juno – Europlanet Society".
  41. ^ Pearson, Ezzy (June 4, 2016). "What will we learn from the Juno mission?". Science Focus. BBC Online. from the original on January 21, 2024.
Notes
  1. The sun orbiting Ulysses' extended mission operation terminated June 30, 2009. The extension permitted a third flyby over the Sun's poles in 2007–2008.
  2. The two Voyager spacecraft continue to operate, with some loss in subsystem redundancy, but retain the capability of returning science data from a full complement of VIM science instruments. Both spacecraft also have adequate electrical power and attitude control propellant to continue operating until around 2020, when the available electrical power will no longer support science instrument operation. At this time, science data return and spacecraft operations will cease.
  3. The Deep Space Positioning System (DSPS) is being developed.

External links and further reading edit

  • JPL DSN – official site.
  • Basics of Space Flight – Chapter 18. Deep Space Network
  • DSN Now, NASA, live status of antennas and spacecraft at all three facilities.
  • Deep Space Communications and Navigation Series – a series of books published by Wiley detailing specifics on the Deep Space Network, JPL's site on [1]
  • Douglas J. Mudgway, Big Dish: Building America's Deep Space Connection to the Planets, University of Florida Press, 2005 ISBN 0-8130-2805-1.
  • (PDF) April 2006 GAO report NASA's Deep Space Network: Current Management Structure Is Not Conducive to Effectively Matching Resources with Future Requirements
  • ESA and NASA extend ties with major new cross-support agreement, on ESA Spacecraft Operations site; retrieved October 19, 2007

nasa, deep, space, network, deep, space, network, redirects, here, other, uses, deep, space, network, disambiguation, network, cost, interplanetary, trajectories, interplanetary, transport, network, worldwide, network, spacecraft, communication, ground, segmen. Deep Space Network redirects here For other uses see Deep Space Network disambiguation For the network of low cost interplanetary trajectories see Interplanetary Transport Network The NASA Deep Space Network DSN is a worldwide network of spacecraft communication ground segment facilities located in the United States California Spain Madrid and Australia Canberra that supports NASA s interplanetary spacecraft missions It also performs radio and radar astronomy observations for the exploration of the Solar System and the universe and supports selected Earth orbiting missions DSN is part of the NASA Jet Propulsion Laboratory JPL Deep Space NetworkInsignia for the Deep Space Network s 50th anniversary celebrations 1963 2013 Alternative namesNASA Deep Space NetworkOrganizationInterplanetary Network Directorate NASA JPL LocationPasadena Los Angeles County California Pacific States RegionCoordinates34 12 6 1 N 118 10 18 W 34 201694 N 118 17167 W 34 201694 118 17167EstablishedOctober 1 1958 1958 10 01 65 years agoWebsitedeepspace wbr jpl wbr nasa wbr govTelescopesGoldstone Deep Space Communications ComplexBarstow California United StatesMadrid Deep Space Communications ComplexRobledo de Chavela Community of Madrid SpainCanberra Deep Space Communication ComplexCanberra Australia Related media on Commons edit on Wikidata Contents 1 General information 1 1 Operations control center 2 Deep space 2 1 Frequency bands 3 History 3 1 DSN and the Apollo program 4 Management 5 Antennas 6 Current signal processing capabilities 7 Network limitations and challenges 8 DSN and radio science 9 See also 10 References 11 External links and further readingGeneral information editMap this section s coordinates using OpenStreetMap Download coordinates as KML GPX all coordinates GPX primary coordinates GPX secondary coordinates nbsp Deep Space Network Operations Center at JPL Pasadena California in 1993 DSN currently consists of three deep space communications facilities located such that a distant spacecraft is always in view of at least one station 1 2 3 They are the Goldstone Deep Space Communications Complex 35 25 36 N 116 53 24 W 35 42667 N 116 89000 W 35 42667 116 89000 Goldstone outside Barstow California For details of Goldstone s contribution to the early days of space probe tracking see Project Space Track the Madrid Deep Space Communications Complex 40 25 53 N 4 14 53 W 40 43139 N 4 24806 W 40 43139 4 24806 Madrid 60 kilometres 37 mi west of Madrid Spain and the Canberra Deep Space Communication Complex CDSCC in the Australian Capital Territory 35 24 05 S 148 58 54 E 35 40139 S 148 98167 E 35 40139 148 98167 Canberra 40 kilometres 25 mi southwest of Canberra Australia near the Tidbinbilla Nature Reserve Each facility is situated in semi mountainous bowl shaped terrain to help shield against radio frequency interference 4 The strategic placement of the stations permits constant observation of spacecraft as the Earth rotates which helps to make the DSN the largest and most sensitive scientific telecommunications system in the world 5 The DSN supports NASA s contribution to the scientific investigation of the Solar System It provides a two way communications link that guides and controls various NASA uncrewed interplanetary space probes and brings back the images and new scientific information these probes collect All DSN antennas are steerable high gain parabolic reflector antennas 4 The antennas and data delivery systems make it possible to 2 acquire telemetry data from spacecraft transmit commands to spacecraft upload software modifications to spacecraft track spacecraft position and velocity perform Very Long Baseline Interferometry observations measure variations in radio waves for radio science experiments gather science data monitor and control the performance of the network Other countries and organizations also run deep space networks The DSN operates according to the standards of the Consultative Committee for Space Data Systems as do most other deep space networks and hence the DSN is able to inter operate with the networks of other space agencies These include the Soviet Deep Space Network the Chinese Deep Space Network the Indian Deep Space Network the Japanese Deep Space Network and the ESTRACK of the European Space Agency These agencies often cooperate for better mission coverage 6 In particular DSN has a cross support agreement with ESA that allows mutual use of both networks for more effectiveness and reduced risk 7 In addition radio astronomy facilities such as Parkes Observatory or the Green Bank Telescope are sometimes used to supplement the antennas of the DSN Operations control center edit Main article Space Flight Operations Facility The antennas at all three DSN Complexes communicate directly with the Deep Space Operations Center also known as Deep Space Network operations control center located at the JPL facilities in Pasadena California 3 In the early years the operations control center did not have a permanent facility It was a provisional setup with numerous desks and phones installed in a large room near the computers used to calculate orbits In July 1961 NASA started the construction of the permanent facility Space Flight Operations Facility SFOF The facility was completed in October 1963 and dedicated on May 14 1964 In the initial setup of the SFOF there were 31 consoles 100 closed circuit television cameras and more than 200 television displays to support Ranger 6 to Ranger 9 and Mariner 4 8 Currently the operations center personnel at SFOF monitor and direct operations and oversee the quality of spacecraft telemetry and navigation data delivered to network users In addition to the DSN complexes and the operations center a ground communications facility provides communications that link the three complexes to the operations center at JPL to space flight control centers in the United States and overseas and to scientists around the world 9 Deep space edit nbsp View from the Earth s north pole showing the field of view of the main DSN antenna locations Once a mission gets more than 30 000 km 19 000 mi from Earth it is al ways in view of at least one of the stations Tracking vehicles in deep space is quite different from tracking missions in low Earth orbit LEO Deep space missions are visible for long periods of time from a large portion of the Earth s surface and so require few stations the DSN has only three main sites These few stations however require huge antennas ultra sensitive receivers and powerful transmitters in order to transmit and receive over the vast distances involved Deep space is defined in several different ways According to a 1975 NASA report the DSN was designed to communicate with spacecraft traveling approximately 16 000 km 10 000 miles from Earth to the farthest planets of the solar system 10 JPL diagrams 11 state that at an altitude of 30 000 km 19 000 mi a spacecraft is always in the field of view of one of the tracking stations Frequency bands edit The International Telecommunication Union which sets aside various frequency bands for deep space and near Earth use defines deep space to start at a distance of 2 million km 1 2 million mi from the Earth s surface 12 These are in S band X band K band and Ka band Because the Moon the Earth moon Lagrange points and the Earth Sun Lagrangian points L1 and L2 are all closer than 2 million km from Earth distances are here they are considered near space and cannot use the ITU s deep space bands History editFurther information History of the Deep Space Network The forerunner of the DSN was established in January 1958 when JPL then under contract to the U S Army deployed portable radio tracking stations in Nigeria Singapore and California to receive telemetry and plot the orbit of the Army launched Explorer 1 the first successful U S satellite 13 NASA was officially established on October 1 1958 to consolidate the separately developing space exploration programs of the US Army US Navy and US Air Force into one civilian organization 14 On December 3 1958 JPL was transferred from the US Army to NASA and given responsibility for the design and execution of lunar and planetary exploration programs using remotely controlled spacecraft Shortly after the transfer NASA established the concept of the Deep Space Network as a separately managed and operated communications system that would accommodate all deep space missions thereby avoiding the need for each flight project to acquire and operate its own specialized space communications network The DSN was given responsibility for its own research development and operation in support of all of its users Under this concept it has become a world leader in the development of low noise receivers large parabolic dish antennas tracking telemetry and command systems digital signal processing and deep space navigation The Deep Space Network formally announced its intention to send missions into deep space on Christmas Eve 1963 it has remained in continuous operation in one capacity or another ever since 15 The largest antennas of the DSN are often called on during spacecraft emergencies Almost all spacecraft are designed so normal operation can be conducted on the smaller and more economical antennas of the DSN but during an emergency the use of the largest antennas is crucial This is because a troubled spacecraft may be forced to use less than its normal transmitter power attitude control problems may preclude the use of high gain antennas and recovering every bit of telemetry is critical to assessing the health of the spacecraft and planning the recovery The most famous example is the Apollo 13 mission where limited battery power and inability to use the spacecraft s high gain antennas reduced signal levels below the capability of the Manned Space Flight Network and the use of the biggest DSN antennas and the Australian Parkes Observatory radio telescope was critical to saving the lives of the astronauts While Apollo was also a US mission DSN provides this emergency service to other space agencies as well in a spirit of inter agency and international cooperation For example the recovery of the Solar and Heliospheric Observatory SOHO mission of the European Space Agency ESA would not have been possible without the use of the largest DSN facilities DSN and the Apollo program edit Although normally tasked with tracking uncrewed spacecraft the Deep Space Network DSN also contributed to the communication and tracking of Apollo missions to the Moon although primary responsibility was held by the Manned Space Flight Network MSFN The DSN designed the MSFN stations for lunar communication and provided a second antenna at each MSFN site the MSFN sites were near the DSN sites for just this reason Two antennas at each site were needed both for redundancy and because the beam widths of the large antennas needed were too small to encompass both the lunar orbiter and the lander at the same time DSN also supplied some larger antennas as needed in particular for television broadcasts from the Moon and emergency communications such as Apollo 13 16 Excerpt from a NASA report describing how the DSN and MSFN cooperated for Apollo 17 Another critical step in the evolution of the Apollo Network came in 1965 with the advent of the DSN Wing concept Originally the participation of DSN 26 m antennas during an Apollo Mission was to be limited to a backup role This was one reason why the MSFN 26 m sites were collocated with the DSN sites at Goldstone Madrid and Canberra However the presence of two well separated spacecraft during lunar operations stimulated the rethinking of the tracking and communication problem One thought was to add a dual S band RF system to each of the three 26 m MSFN antennas leaving the nearby DSN 26 m antennas still in a backup role Calculations showed though that a 26 m antenna pattern centered on the landed Lunar Module would suffer a 9 to 12 db loss at the lunar horizon making tracking and data acquisition of the orbiting Command Service Module difficult perhaps impossible It made sense to use both the MSFN and DSN antennas simultaneously during the all important lunar operations JPL was naturally reluctant to compromise the objectives of its many uncrewed spacecraft by turning three of its DSN stations over to the MSFN for long periods How could the goals of both Apollo and deep space exploration be achieved without building a third 26 m antenna at each of the three sites or undercutting planetary science missions The solution came in early 1965 at a meeting at NASA Headquarters when Eberhardt Rechtin suggested what is now known as the wing concept The wing approach involves constructing a new section or wing to the main building at each of the three involved DSN sites The wing would include a MSFN control room and the necessary interface equipment to accomplish the following Permit tracking and two way data transfer with either spacecraft during lunar operations Permit tracking and two way data transfer with the combined spacecraft during the flight to the Moon Provide backup for the collocated MSFN site passive track spacecraft to ground RF links of the Apollo spacecraft during trans lunar and trans earth phases With this arrangement the DSN station could be quickly switched from a deep space mission to Apollo and back again GSFC personnel would operate the MSFN equipment completely independently of DSN personnel Deep space missions would not be compromised nearly as much as if the entire station s equipment and personnel were turned over to Apollo for several weeks The details of this cooperation and operation are available in a two volume technical report from JPL 18 19 Management editThe network is a NASA facility and is managed and operated for NASA by JPL which is part of the California Institute of Technology Caltech The Interplanetary Network Directorate IND manages the program within JPL and is charged with the development and operation of it The IND is considered to be JPL s focal point for all matters relating to telecommunications interplanetary navigation information systems information technology computing software engineering and other relevant technologies While the IND is best known for its duties relating to the Deep Space Network the organization also maintains the JPL Advanced Multi Mission Operations System AMMOS and JPL s Institutional Computing and Information Services ICIS 20 21 The facilities in Spain and Australia are jointly owned and operated in conjunction with that government s scientific institutions In Australia the Commonwealth Scientific and Industrial Research Organisation CSIRO an Australian Commonwealth Government Statutory Authority established the CSIRO Astronomy and Space Science Division to manage the day to day operations engineering and maintenance activities of the Canberra Deep Space Communications Complex 22 Most of the staff at Tidbinbilla are Australian government employees the land and buildings are owned by the Australian government NASA provides the bulk of the funding owns the movable property such as dishes and electronic equipment which it has paid for and gets to decide where to point the dishes 23 Similarly in Spain Ingenieria de Sistemas para la Defensa de Espana S A ISDEFE a wholly owned subsidiary of the Instituto Nacional de Tecnica Aeroespacial INTA and a part of the Spanish Department of Defense operates and maintains the Madrid Deep Space Communications Complex Madrid 22 Peraton formerly Harris Corporation is under contract to JPL for the DSN s operations and maintenance Peraton has responsibility for managing the Goldstone complex operating the DSOC and for DSN operations mission planning operations engineering and logistics 24 25 26 Antennas edit nbsp 70 m antenna at Goldstone California Each complex consists of at least four deep space terminals equipped with ultra sensitive receiving systems and large parabolic dish antennas There are Three or more 34 meter 112 ft Beam waveguide antennas BWG One 70 meter 230 ft antenna Five of the 34 meter 112 ft beam waveguide antennas were added to the system in the late 1990s Three were located at Goldstone and one each at Canberra and Madrid A second 34 meter 112 ft beam waveguide antenna the network s sixth was completed at the Madrid complex in 2004 In order to meet the current and future needs of deep space communication services a number of new Deep Space Station antennas had to be built at the existing Deep Space Network sites At the Canberra Deep Space Communication Complex the first of these was completed in October 2014 DSS35 with a second becoming operational in October 2016 DSS36 27 A new 34 meter dish DSS53 became operational at the Madrid complex in February 2022 28 By 2025 the 70 meter antennas at all three locations will be decommissioned and replaced with 34 meter BWG antennas that will be arrayed All systems will be upgraded to have X band uplink capabilities and both X and Ka band downlink capabilities 29 Current signal processing capabilities edit nbsp The Canberra Deep Space Communication Complex in 2008The general capabilities of the DSN have not substantially changed since the beginning of the Voyager Interstellar Mission in the early 1990s However many advancements in digital signal processing arraying and error correction have been adopted by the DSN The ability to array several antennas was incorporated to improve the data returned from the Voyager 2 Neptune encounter and extensively used for the Galileo mission when the spacecraft s high gain antenna failed to deploy and as a result Galileo was forced to resort to operating solely off its low gain antennas 30 The DSN array currently available since the Galileo mission can link the 70 meter 230 ft dish antenna at the Deep Space Network complex in Goldstone California with an identical antenna located in Australia in addition to two 34 meter 112 ft antennas at the Canberra complex The California and Australia sites were used concurrently to pick up communications with Galileo Arraying of antennas within the three DSN locations is also used For example a 70 meter 230 ft dish antenna can be arrayed with a 34 meter dish For especially vital missions like Voyager 2 non DSN facilities normally used for radio astronomy can be added to the array 31 In particular the Canberra 70 meter 230 ft dish can be arrayed with the Parkes Radio Telescope in Australia and the Goldstone 70 meter dish can be arrayed with the Very Large Array of antennas in New Mexico 32 Also two or more 34 meter 112 ft dishes at one DSN location are commonly arrayed together All the stations are remotely operated from a centralized Signal Processing Center at each complex These Centers house the electronic subsystems that point and control the antennas receive and process the telemetry data transmit commands and generate the spacecraft navigation data Once the data are processed at the complexes they are transmitted to JPL for further processing and for distribution to science teams over a modern communications network Especially at Mars there are often many spacecraft within the beam width of an antenna For operational efficiency a single antenna can receive signals from multiple spacecraft at the same time This capability is called Multiple Spacecraft Per Aperture or MSPA Currently the DSN can receive up to 4 spacecraft signals at the same time or MSPA 4 However apertures cannot currently be shared for uplink When two or more high power carriers are used simultaneously very high order intermodulation products fall in the receiver bands causing interference to the much 25 orders of magnitude weaker received signals 33 Therefore only one spacecraft at a time can get an uplink though up to 4 can be received Network limitations and challenges edit nbsp 70m antenna in Robledo de Chavela Community of Madrid SpainThere are a number of limitations to the current DSN and a number of challenges going forward The Deep Space Network nodes are all on Earth Therefore data transmission rates from to spacecraft and space probes are severely constrained due to the distances from Earth For now it can connect with the Mars orbiters in the Mars Relay Network for faster and more flexible communications with spacecraft and landers on Mars 34 Adding dedicated communication satellites elsewhere in space to handle multiparty multi mission use such as the canceled Mars Telecommunications Orbiter would increase flexibility towards some sort of Interplanetary Internet The need to support legacy missions that have remained operational beyond their original lifetimes but are still returning scientific data Programs such as Voyager have been operating long past their original mission termination date They also need some of the largest antennas Replacing major components can cause problems as it can leave an antenna out of service for months at a time The older 70 m antennas are reaching the end of their lives At some point these will need to be replaced The leading candidate for 70 m replacement had been an array of smaller dishes 35 36 but more recently the decision was taken to expand the provision of 34 meter 112 ft BWG antennas at each complex to a total of 4 37 All the 34 meter HEF antennas have been replaced New spacecraft intended for missions beyond geocentric orbits are being equipped to use the beacon mode service which allows such missions to operate without the DSN most of the time 38 DSN and radio science edit nbsp Illustration of Juno and Jupiter Juno is in a polar orbit that takes it close to Jupiter as it passes from north to south getting a view of both poles During the GS experiment it must point its antenna at the Deep Space Network on Earth to pick up a special signal sent from DSN The DSN forms one portion of the radio sciences experiment included on most deep space missions where radio links between spacecraft and Earth are used to investigate planetary science space physics and fundamental physics The experiments include radio occultations gravity field determination and celestial mechanics bistatic scattering doppler wind experiments solar corona characterization and tests of fundamental physics 39 For example the Deep Space Network forms one component of the gravity science experiment on Juno This includes special communication hardware on Juno and uses its communication system 40 The DSN radiates a Ka band uplink which is picked up by Juno s Ka Band communication system and then processed by a special communication box called KaTS and then this new signal is sent back the DSN 40 This allows the velocity of the spacecraft over time to be determined with a level of precision that allows a more accurate determination of the gravity field at planet Jupiter 40 41 Another radio science experiment is REX on the New Horizons spacecraft to Pluto Charon REX received a signal from Earth as it was occulted by Pluto to take various measurements of that system of bodies See also editExtended NASA missionsMars Science Laboratory Curiosity rover Perseverance rover Voyager program Heliosheath and Heliopause Voyager 1 Voyager 2 International Cometary Explorer Earth s magnetic field and Solar wind New Horizons Pluto James Webb Space Telescope Related Sources and TopicsSpace Network Near Earth Network Space Communications and Navigation Program SCaN Tracking and Data Relay Satellite List of observatories List of radio telescopesReferences edit Haynes Robert 1987 How We Get Pictures From Space PDF NASA Facts Revised ed NASA Archived PDF from the original on April 18 2022 Retrieved September 19 2013 a b About the Deep Space Network JPL Archived from the original on 2012 06 08 Retrieved 2012 06 08 a b Latifiyan Pouya April 2021 Space Telecommunications how Take off 1 Tehran Civil Aviation Technology College 15 via Persian a b DSN antennas JPL NASA Archived from the original on 2011 04 11 Bracing for an Interplanetary Traffic Jam science nasa gov NASA Archived from the original on May 15 2017 Retrieved May 17 2018 Susan Kurtik 23 April 2013 Deep Space Network DSN Mission Services and Operations Interface for Small Deep Space Missions PDF Jet Propulsion Laboratory hdl 2014 44347 S2CID 117882864 Archived PDF from the original on 2022 04 18 Warhaut Manfred Braukus Michael April 2 2007 ESA and NASA extend ties with major new cross support agreement www esa int Press release ESA Archived from the original on February 5 2023 Retrieved July 5 2020 Deep Space Network Operations Control Center at the Jet Propulsion Laboratory Pasadena California Picture Album of the DEEP SPACE NETWORK NASA JPL Archived from the original on 17 February 2013 Retrieved 26 January 2014 NASA Facts Deep Space Network PDF JPL Archived from the original PDF on 2020 04 26 Retrieved 2011 03 25 Renzetti N May 1975 DSN Functions and Facilities PDF Technical report JPL Archived PDF from the original on September 3 2023 Deutsch Les June 24 2012 NASA s Deep Space Network Big Antennas with a Big Job Anten Sympoisum Toulouse Space Show PDF Toulouse France JPL p 25 hdl 2014 42668 Archived from the original on January 21 2024 201 Rev B Frequency and Channel Assignments PDF December 15 2009 Archived from the original PDF on June 11 2014 Retrieved July 13 2014 Mudgway Douglas J 2001 Uplink Downlink A History of the Deep Space Network 1957 1997 PDF p 5 SP 2001 4227 Archived PDF from the original on April 11 2023 NASA 2005 The National Aeronautics and Space Act NASA Retrieved November 9 2007 Stirone Shannon March 2018 Welcome to the Center of the Universe LongReads Archived from the original on December 2 2023 Retrieved March 17 2018 Soumyajit Mandal Engineering Apollo Interview Report Deep Space Network Support for the Apollo Missions PDF Archived from the original PDF on July 20 2011 Retrieved July 2 2008 William R Corliss June 1974 NASA Technical report CR 140390 Histories of the Space Tracking and Data Acquisition Network STADAN the Manned Space Flight Network MSFN and the NASA Communications Network NASCOM PDF Report NASA hdl 2060 19750002909 Archived PDF from the original on 2022 03 03 100MB PDF file Explicitly non copyrighted Flanagan F M Goodwin P S Renzetti N A July 15 1970 Deep Space Network Support of the Manned Space Flight Network for Apollo 1962 1968 PDF Technical report Vol 1 NASA JPL TM 33 452 VOL 1 NASA CR 116801 Archived PDF from the original on May 21 2022 Flanagan F M Goodwin P S Renzetti N A May 1971 Deep Space Network Support of the Manned Space Flight Network for Apollo 1969 1970 PDF Technical report Vol 2 NASA JPL TM 33 452 VOL 2 NASA CR 118325 Archived PDF from the original on April 18 2022 IND Technology Program Overview JPL Archived from the original on 2009 04 11 Weber William J May 27 2004 Interplanetary Network Directorate 7th Briefing for Industry PDF Pasadena California JPL hdl 2014 40704 Archived from the original on January 21 2024 a b NASA S MANAGEMENT OF THE DEEP SPACE NETWORK PDF Agreement between the Government of Australia and the Government of the United States of America for Space Vehicle Tracking and Communication Facilities Lackey Leah May 23 2013 ITT Exelis selected for NASA Deep Space Network subcontract by Jet Propulsion Laboratory Press release ITT Exelis Archived from the original on January 21 2024 Retrieved July 5 2016 via SpaceRef Gelles David February 6 2015 Harris Corporation to Buy Defense Contractor Exelis for 4 7 Billion DealBook The New York Times Archived from the original on March 26 2023 Retrieved October 31 2016 CONTRACT to PERATON INC USAspending Retrieved 2023 05 15 Antennas NASA Archived from the original on June 6 2023 Retrieved July 13 2015 O Neill Ian J Pamer Melissa NASA Adds Giant New Dish to Communicate with Deep Space Network Press release JPL Archived from the original on January 17 2024 Retrieved November 17 2022 Proposed DSN Aperture Enhancement Project Transition nasa gov May 16 2018 Archived from the original on February 5 2015 Retrieved May 16 2018 Uplink Downlink Chapter 5 The Galileo Era 1986 1996 Brown D W Brundage W D Ulvestad J S Kent S S Bartos K P August 15 1990 Interagency Telemetry Arraying for the Voyager Neptune Encounter PDF Technical report JPL TDA Progress Report 42 102 Archived PDF from the original on November 17 2023 Antenna Arraying JPL 30 March 2020 Conroy B L Hoppe D J November 15 1996 Noise Bursts and Intermodulation Products Caused by Multiple Carriers at X Band PDF Technical report JPL TDA Progress Report 42 127 Archived PDF from the original on December 6 2023 O Neill Ian J Hautaluoma Grey Johnson Alana February 16 2021 The Mars Relay Network Connects Us to NASA s Martian Explorers NASA s Mars Exploration Program Press release NASA Archived from the original on January 11 2024 Retrieved March 10 2021 The Future Deep Space Network An Array of Many Small Antennas JPL Archived from the original on July 14 2009 Durgadas S Bagri Joseph I Statman amp Mark S Gatti 2007 Proposed Array Based Deep Space Network for NASA Proceedings of the IEEE 95 10 IEEE 1916 1922 doi 10 1109 JPROC 2007 905046 S2CID 27224753 DSN Aperature Enhancement Project NASA November 10 2012 Archived from the original on February 5 2015 Retrieved June 6 2013 Wyatt E Jay Foster Mike Schlutsmeyer Alan Sherwood Rob Sue Miles K An Overview of the Beacon Monitor Operations Technology PDF Technical report JPL Archived PDF from the original on March 21 2023 Radio Science JPL Archived from the original on 2016 12 03 a b c European Involvement in Juno Europlanet Society Pearson Ezzy June 4 2016 What will we learn from the Juno mission Science Focus BBC Online Archived from the original on January 21 2024 NotesThe sun orbiting Ulysses extended mission operation terminated June 30 2009 The extension permitted a third flyby over the Sun s poles in 2007 2008 The two Voyager spacecraft continue to operate with some loss in subsystem redundancy but retain the capability of returning science data from a full complement of VIM science instruments Both spacecraft also have adequate electrical power and attitude control propellant to continue operating until around 2020 when the available electrical power will no longer support science instrument operation At this time science data return and spacecraft operations will cease The Deep Space Positioning System DSPS is being developed External links and further reading edit nbsp Wikimedia Commons has media related to Deep Space Network JPL DSN official site Basics of Space Flight Chapter 18 Deep Space Network DSN Now NASA live status of antennas and spacecraft at all three facilities Deep Space Communications and Navigation Series a series of books published by Wiley detailing specifics on the Deep Space Network JPL s site on 1 Douglas J Mudgway Big Dish Building America s Deep Space Connection to the Planets University of Florida Press 2005 ISBN 0 8130 2805 1 PDF April 2006 GAO report NASA s Deep Space Network Current Management Structure Is Not Conducive to Effectively Matching Resources with Future Requirements An Early NASA Pioneer Still on the Job in Deep Space ESA and NASA extend ties with major new cross support agreement on ESA Spacecraft Operations site retrieved October 19 2007 Retrieved from https en wikipedia org w index php title NASA Deep Space Network amp oldid 1205277901, wikipedia, wiki, book, books, library,

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