Dawn At Ceres

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Press Kit/March 2015Dawn at Ceres

ContentsMedia Contacts & Services . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Quick Facts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4About the Dawn mission . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6Why Dawn? . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6Top Findings at Vesta . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7Mission Science Objectives . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7Dawn at Ceres . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8About Ceres . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8Ceres Activity Plan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9Ceres Timeline . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9Spacecraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11Structure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11Telecommunication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11Ion Propulsion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11Solar Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12Science Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12Program & Project Management . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14NASA’s Discovery Program . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14Appendix: Selected Images & Videos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

Media Contacts & ServicesDwayne BrownPolicy and Program202-358-1726NASA ington, DCElizabeth Landau/Preston DychesDawn Mission Management818-354-6425/818-354-7013NASA’s Jet Propulsion Laboratory,and Operationselizabeth.landau@jpl.nasa.govPasadena, Californiapreston.dyches@jpl.nasa.govStuart WolpertUCLALos Angeles, CaliforniaScience InvestigationLeadership: Dawn’sPrincipal irgit KrummheuerFraming CameraMax Planck Institute forSolar System ResearchGöttingen, Germany 49 0551 384 979-462Krummheuer@mps.mpg.deManuela BraunFraming CameraGerman Aerospace Center (DLR)Institute of Planetary ResearchCologne, Germany 49 02203 601-3882Manuela.Braun@dlr.deEnrico FlaminiVisible and infraredItalian Space Agencymapping spectrometerRome, ItalyEnrico.Flamini@asi.itLivia GiacominiVisible and infrared mapping 3906/49934052Italian National Institute for csRome, ItalyAlan FischerGamma ray and neutron detectorPlanetary Science InstituteTucson, ArizonaDeanna WilkeBuilt spacecraftOrbital ATK, Inc.Griffin Communications GroupDulles, VirginiaDawn at a@griffincg.comPress Kit

Media Services InformationNASA Television TransmissionInternet ResourcesNASA Television Channels are MPEG-2 digital Cband signals, carried by QPSK/DVB-S modulation onsatellite AMC-18C, transponder 3C, at 105 degreeswest longitude, with a downlink frequency of 3760MHz, vertical polarization, data rate of 38.80 MHz,symbol rate of 28.0681 Mbps, and 3/4 FEC. A DigitalVideo Broadcast (DVB) compliant Integrated Receiver Decoder (IRD) is needed for reception.News and information about the Dawn mission,including an electronic copy of this press kit,news releases, fact sheets, status reports andimages, are available from the NASA Web site athttp://www.nasa.gov/dawn.Detailed background information on the missionis available from the Dawn project home page athttp://dawn.jpl.nasa.gov.For digital downlink information for NASA TV’s MediaChannel, access to NASA TV’s Public Channel onthe Web and a schedule of programming for Dawnlaunch activities, visit http://www.nasa.gov/nasatv.News conferenceA preview news conference to discuss Dawn’s approach to Ceres and planned operations at the dwarfplanet will be held at NASA’s Jet Propulsion Laboratory at noon EST (9 a.m. PST) on March 2, 2015.The briefing will be carried live on NASA Televisionand on voice circuits.Dawn at Ceres3Press Kit

Quick FactsSpacecraftWeight: 20 pounds (8.9 kilograms) eachDimensions: The spacecraft bus is 5.4 feet(1.64 meters) long, 4.2 feet (1.27 meters) wide and5.8 feet (1.77 meters) high. High-gain antenna is5 feet (1.52 meters) in diameter. When the solararrays are deployed, Dawn’s wingspan is 64 feet,9 inches (19.7 meters).Fuel: 937 pounds (425 kilograms) of xenonpropellant at launchFuel remaining at Ceres orbit entry: 88 pounds(40 kilograms)Spacecraft acceleration via ion propulsion:0 to 60 mph in four daysWeight: 2,684.6 pounds (1,217.7 kilograms) atlaunch, consisting of 1,647.1-pound (747.1-kilogram)spacecraft, 937 pounds (425 kilograms) xenon propellant and 100.5 pounds (45.6 kilograms) hydrazinepropellant.Thrust: 0.07 to 0.33 ounce (19 to 91 millinewtons)Estimated days of thrusting for entire mission:2,000Power: Two 27-foot-by-7-foot (8.3-meter-by2.3-meter) solar panels, together providing more than10 kilowatts, depending on distance from the sun.Days of thrusting up to orbit at Ceres: 1,885Each wing weighs almost 139 pounds(63 kilograms).MissionLaunch: Sept. 27, 2007Power storage via 35-amp-hour rechargeable nickelhydrogen batteryLaunch site: Cape Canaveral Air Force Station, Fla.,Pad 17BNumber of science instruments: 3Launch vehicle: Delta II Heavy 2925H-9.5 includingStar 48 upper stageIon Propulsion SystemMars gravity assist: Feb. 17, 2009Number of thrusters: 3Vesta arrival: July 16, 2011Thruster dimensions (each): 13 inches (33 centimeters) long, 12 inches (30 centimeters) in diameterCeres’ distance to Earth at time of Dawn arrival:310 million miles (500 million kilometers)Dawn at Ceres4Press Kit

Dawn FirstsDistance traveled by spacecraft launch-to-Vesta:1.7 billion miles (2.8 billion kilometers)Vesta departure: Sept. 5, 2012Dawn’s mission to Ceres and Vesta is unique for thefollowing reasons:Ceres arrival: March 6, 2015 Dawn is the first mission to visit Ceres and thefirst mission to visit Vesta.Distance spacecraft travels between Vesta andCeres: 920 million miles (1.5 billion kilometers) Dawn is the first spacecraft to orbit two extraterrestrial targets When Dawn arrives at Ceres in March 2015, itwill be the first spacecraft to visit a dwarf planet.(New Horizons flies by Pluto, another dwarfplanet, in July 2015.) A dwarf planet is round andorbits the sun, but is unable to clear its orbitalpath such that there are no similar objects atroughly the same distance from the sun. When Dawn visited Vesta, it also became the firstspacecraft to orbit a main-belt asteroid.Total distance spacecraft travels from Earth toVesta to Ceres: 3.1 billion miles (4.9 billionkilometers)End of primary mission: June 2016Program Cost: 472 million total, including 373 million to build and launch the spacecraftand 99 million for 10 years of operations anddata analysis.Ceres is the largest, most massive object in themain asteroid belt, with an average diameter ofabout 590 miles (950 kilometers).Vesta is 326 miles (525 kilometers) in diameter andthe second most massive object in the asteroid belt.*Additional facts about cfm?Object Dwa Ceres&Display FactsDawn at Ceres5Press Kit

About the Dawn missionate a picture of the early solar system history in theregion of the main asteroid belt. Data returned fromthe Dawn spacecraft could contribute to significantbreakthroughs in our understanding of how the solarsystem formed.Why Dawn?NASA’s Dawn spacecraft is on a mission to study thetwo most massive objects in the main asteroid beltbetween Mars and Jupiter, Vesta and Ceres. Studying these worlds allows scientists to do historicalresearch in space, opening a window into the earliestchapter in the history of our solar system. At eachtarget, Dawn acquires color photographs, maps theelemental and mineralogical composition, measuresthe gravity field and searches for moons.To carry out its scientific mission, the Dawn spacecraft will conduct four science experiments producingdata that will be used in combination to characterize these bodies. Dawn carries a pair of visible-lightcameras (one prime and one backup), a visible andinfrared mapping spectrometer, and a gamma ray andneutron spectrometer. Radio and optical navigationdata will provide information about the gravity field,and thus bulk properties and internal structure, of thetwo bodies.The data gathered by Dawn will enable scientists tounderstand the conditions under which these objectsformed, determine the nature of the building blocksfrom which the terrestrial planets (like Earth) formed,and contrast the formation and evolution of Vesta andCeres.Dawn’s mission to Vesta and Ceres is managed bythe Jet Propulsion Laboratory for NASA’s ScienceMission Directorate in Washington. Dawn is a projectof the directorate’s Discovery Program, managed byNASA’s Marshall Space Flight Center in Huntsville, Alabama. UCLA is responsible for overall Dawn missionscience. Orbital ATK, Inc., of Dulles, Virginia, designedand built the spacecraft. JPL is managed for NASAby the California Institute of Technology in Pasadena.Dawn’s quest to understand the conditions that existed when our solar system formed provides contextfor the observation of planetary systems around otherstars. Vesta and Ceres are the two largest survivingintact asteroids. Their special qualities are explainedby the processes at work during the earliest chaptersof our solar system’s history, when the materials in thesolar nebula (a disk around the sun that formed fromdust and hydrogen gas) varied with their distancefrom the sun. As this distance increased, the temperature dropped, with terrestrial bodies forming closerto the sun, and icy bodies forming farther away.The Framing Cameras were provided by the MaxPlanck Institute for Solar System Research, Göttingen, Germany, with significant contributions by theGerman Aerospace Center (DLR) Institute of Planetary Research, Berlin, and in coordination with theInstitute of Computer and Communication NetworkEngineering, Braunschweig. The visible and infraredmapping spectrometer was funded and coordinatedby the Italian Space Agency and built by SELEX ES,with the scientific leadership of the Institute for SpaceAstrophysics and Planetology, Italian National Institutefor Astrophysics, Italy, and is operated by the Institutefor Space Astrophysics and Planetology, Rome, Italy.The gamma ray and neutron detector was built byLos Alamos National Laboratory, New Mexico, and isoperated by the Planetary Science Institute, Tucson,Arizona.Vesta and Ceres straddle a boundary in the asteroidbelt between primarily rocky bodies and ice-bearingbodies. They present contrasting stories of fire andice. Vesta is a dry, differentiated object, shaped byvolcanism, with a crust that shows signs of resurfacing. Ceres, by contrast, has a surface containinglower-temperature water-bearing minerals, and maypossess a very tenuous atmosphere.By studying both of these two distinct bodies withthe same complement of instruments on the samespacecraft, the Dawn mission hopes to comparethe different evolutionary path each took, and cre-Dawn at Ceres6Press Kit

Top Findings at VestaData from Dawn revealed the presence of anomalousdark spots and streaks on Vesta’s surface, whichcorrespond to dark inclusions found in meteoritesfrom Vesta, which were likely deposited by ancientasteroid impacts. Based on measurements of itsmass, shape, volume and spin state with radiometryand imagery, Dawn confirmed the presence of a coreinside Vesta and placed constraints on its size.Researchers continue to examine data collected byDawn for additional insights into the formation andhistory of Vesta. Dawn data can be accessed bythe public at http://dawndata.igpp.ucla.edu andthrough NASA’s Planetary Data System.Mission Science Objectives Test the scientific theory that Vesta is the parent body for a class of stony meteorites knownas howardite, eucrite and diogenite meteorites;determine which, if any, meteorites come fromCeres. Provide a geologic context for howardite, eucriteand diogenite meteorites (at Vesta). Obtain surface coverage with the mapping spectrometer from 0.4- to 5.0-micron wavelengths. Obtain neutron and gamma ray spectra to produce maps of the surface elemental compositionof each object, including the abundance of majorrock-forming elements (oxygen, magnesium, aluminum, silicon, calcium, titanium and iron), traceelements (gadolinium and samarium), and longlived radioactive elements (potassium, thoriumand uranium).In particular, the mission’s scientific objectives are to: Investigate the internal structure, density andhomogeneity of two complementary protoplanets— one wet (Ceres) and one dry (Vesta). Determine surface shape and cratering via nearglobal surface imagery in three colors at Vestaand at Ceres. Perform radio tracking to determine mass, gravityfield, principal axes, rotational axis and momentsof inertia of both Vesta and Ceres. Determine shape, size, composition and mass ofVesta and Ceres. Determine thermal history and size of each body’score. Determine the spin axis of Vesta and Ceres. Understand the role of water in controllingasteroid evolution.Dawn at CeresThis graphic shows Dawn’s path to Vesta and Ceres with the spacecraft’slocation on September 27 of various years.7Press Kit

Dawn at Cerescontains large amounts of water ice beneath itssurface. In 2014, scientists using the Herschel SpaceObservatory found evidence for water vapor beingemitted by Ceres. The vapor may be producedby cryovolcanoes or by ice near the surface sublimating (transforming from solid to gas).Spectral characteristics of Ceres from ground-basedtelescopic data suggest it has a surface compositionsimilar to that of meteorites known as carbonaceouschondrites. In January 2014, emissions of watervapor were detected from several regions of Ceres.Dawn will explore the dwarf planet Ceres with thesame complement of instruments used in its visit toVesta. In-depth analysis and comparison of these twocelestial bodies will provide insight into their origin andevolution — and thus give us a better understandingof the conditions and processes that have acted uponthem since their formation 4.56 billion years ago.Astronomers estimate that if Ceres were composedof 25 percent water, it might have more water thanall the fresh water on Earth. Ceres’ water, unlike thatfound on Earth, cannot remain liquid on the surface. The water is located in the mantle beneath thesurface in the form of liquid water, ice and hydratedrock.During its orbital studies, Dawn will investigate theinternal structure, density and homogeneity of Ceresby measuring its mass, shape, volume and spin statewith radiometric tracking and imagery. It will determine the dwarf planet’s elemental and mineral composition. From this information, scientists can explorethe possible relationship between meteorites andCeres, and the thermal histories of the dwarf planet.From images of the surface, knowledge of Ceres’bombardment, and its tectonic, and possibly volcanic, history will be revealed.Observations by NASA’s Hubble Space Telescopeshow that Ceres shares characteristics of the rocky,terrestrial planets of our inner solar system. Computermodels show that nearly round objects such as Ceres have a differentiated interior, with denser materialat the core and lighter minerals near the surface. Allthe terrestrial planets — including Earth — have differentiated interiors. This sets Ceres and Vesta apartfrom most of their asteroid neighbors.DiscoveryAbout CeresCeres was the first object discovered in the asteroidbelt. Sicilian astronomer Father Giuseppe Piazzi spotted the object in 1801. As more such objects werefound in the same region, they became known asasteroids or minor planets. Ceres was initially classified as a planet and later classified as an asteroid.In recognition of its planet-like qualities, Ceres wasdesignated a dwarf planet in 2006 along with Plutoand Eris.Scientists describe Ceres as an “embryonic planet.”Gravitational perturbations from Jupiter billions ofyears ago prevented the formation of a terrestrialsized planet between itself and Mars. Ceres endedup among the leftover debris of planetary formation inthe region now known as the main asteroid belt.NASA’s Hubble Space Telescope observed Ceres’rotation, demonstrating that it is nearly round. LikeEarth, Ceres’ diameter at its equator is wider than atits poles. On average, Ceres is approximately 590miles (950 kilometers) across. Ceres comprises 25percent or more of the asteroid belt’s total mass.How Ceres Got its NameCeres is named for the Roman goddess of agricultureand harvests. Craters on Ceres will be named forgods and goddesses of agriculture and vegetationfrom world mythology. Other features will be namedfor agricultural festivals.But Ceres has more in common with Earth and Marsthan its rocky neighbors. There are signs that CeresDawn at Ceres8Press Kit

Dawn’s Ceres Activity Planand to perform a gravity investigation. GRaND willreveal the signatures of the elements on and nearthe surface. The gravity experiment will measurethe tug of the dwarf planet, as monitored by changes in the high-precision radio link to NASA’s DeepSpace Network of antennas on Earth.Ceres Approach and ArrivalAs it did at Vesta, Dawn will use its ion propulsionto make a slow approach to drop into orbit aroundCeres. The approach phase began in December2014, and will conclude when Dawn achieves itsfirst planned science observation orbit around Ceresin April 2015. On March 6, 2015, at a distance of41,000 miles (61,000 kilometers), Ceres’ gravity willgently capture Dawn into orbit.End of MissionThe resource that will ultimately limit Dawn’s lifetimeis its hydrazine fuel. Once the fuel is exhausted, thespacecraft will no longer be able to point its instruments at the surface. It also will be unable to pointany of its ion engines for maneuvering purposes,nor point its antenna at Earth or its solar arrays atthe sun. The battery will be depleted in a matter ofhours. The spacecraft will remain in orbit aroundCeres, but it will cease operating.Ceres OrbitThe 14-month prime science phase will run fromApril 2015 through June 2016. As at Vesta, Dawn willnavigate a series of near-circular, near-polar orbits ofdifferent altitudes and orientations that will providevantage points for studying nearly the entire surfaceof Ceres.Planetary ProtectionAsteroids and dwarf planets are bodies that are ofintense interest to the study of organic chemistryand the origin of life, but are not typically believed tobe vulnerable to contamination by Earth-origin microorganisms. However, the potential for the presence of water ice on Ceres prompted the NASAPlanetary Protection Office to impose a requirementthat the spacecraft not impact Ceres for at least 20years after completion of the nominal mission. Tobe conservative, the Dawn project team chose anorbit that will not impact Ceres for at least 50 years.Dawn will make its first full scientific characterization of Ceres in April and May 2015, at an altitude ofabout 8,400 miles (13,500 kilometers); this phase iscalled the Rotation Characterization #3 (RC3) orbit.Then, it will spiral down to an altitude of about 2,750miles (4,430 kilometers), and obtain more sciencedata in its survey science orbit. This phase will last for22 days and is designed to obtain an improved globalview of Ceres with the camera and the visible andinfrared mapping spectrometer (VIR).Dawn will then continue to spiral down to an altitudeof about 920 miles (1,480 kilometers), and in August2015, will begin a two-month phase known as thehigh-altitude mapping orbit, or HAMO. During thisphase, the spacecraft will continue to acquire nearglobal maps with VIR and the camera at higher resolution than in the survey phase. The spacecraft alsowill image in “stereo” to resolve the surface in 3-D.Ceres TimelineThen, after spiraling closer to Ceres for two moremonths, Dawn will begin its nearest orbit around Ceres in late November, at a distance of about 230 miles(375 kilometers). This low-altitude mapping orbit, orLAMO, is specifically designed to acquire data withDawn’s gamma ray and neutron detector (GRaND)Dawn at Ceres9SciencePhaseStart DateEnd DateApproachDec. 26, 2014April 23, 2015CaptureMarch 6, 2015RC3April 23, 2015May 9, 20158,400 miles(13,500 km)20SurveyJune 6, 2015June 30, 20152,730 miles(4,400 km)22HAMOAug. 4, 2015Oct. 15, 2015910 miles(1,470 km)56LAMODec. 15, 2015June 30, 2016230 miles(375 0041,000 miles(61,000 km)Press Kit

Dawn science orbits at CeresThese diagrams show Dawn’s spiraling transitions to increasinglylower orbits. Left to right: RC3 orbit to survey orbit, survey orbitto HAMO and HAMO to LAMO. In the latter two figures, dark bluerepresents time spent in higher orbits and red represents time inlower orbits.Dawn at Ceres10Press Kit

SpacecraftEach of Dawn’s three 12-inch (30-centimeter) diameter ion thrust units is movable in two axes to allow formigration of the spacecraft’s center of mass duringthe mission. This also allows the attitude control system to use the ion thrusters to help control spacecraftattitude.The Dawn spacecraft combines innovative stateof-the-art technologies pioneered by other recentmissions with off-the-shelf components and, in somecases, spare parts and instrumentation left over fromprevious missions.Most systems on the spacecraft have a backupavailable if the main system encounters a problem.Automated onboard fault protection software willsense any unusual conditions and attempt to switchto backups.Three ion propulsion engines are required to provideenough thruster lifetime to complete the missionand still have adequate reserve. However, only onethruster operates at any given time. Dawn has usedion propulsion for years at a time, with interruptionsof only a few hours each week to turn to point thespacecraft’s antenna to Earth.With its wide solar arrays extended, Dawn is aboutas long as a tractor-trailer at 65 feet (19.7 meters).The thrusters work by using an electrical charge toaccelerate ions from xenon fuel to a speed sevento 10 times that of chemical engines. The electrical power level and xenon fuel feed can be adjustedto throttle each engine up or down in thrust. Theengines are thrifty with fuel, using only about 3.25 milligrams of xenon per second (about 10 ounces over24 hours) at maximum thrust. The Dawn spacecraftcarried 937 pounds (425 kilograms) of xenon propellant at launch.StructureThe core of the Dawn spacecraft’s structure is agraphite composite cylinder. Tanks for the ion engines’ xenon gas and the conventional thrusters’hydrazine are mounted inside the cylinder. The cylinder is surrounded by panels made of aluminum corewith aluminum facesheets; most of the other hardware is mounted on these panels. Access panels andother spacecraft panels have composite or aluminumfacesheets and aluminum cores. Blankets, surfaceradiators, finishes and heaters control the spacecraft’stemperature.TelecommunicationThe telecommunication subsystem provides communication with Earth through any of three low-gainantennas and one 5-foot (1.52-meter) diameterparabolic high-gain antenna. The high-gain antennais the primary one used for most communication. Thelow-gain antennas are used when the spacecraft isnot pointing the high-gain antenna toward Earth. Onlyone antenna can be used at a time.Ion PropulsionIon Propulsion SystemDawn’s futuristic, hyper-efficient ion propulsion system allows Dawn to go into orbit around two different extraterrestrial targets, a first for any spacecraft.Meeting the ambitious mission objectives would beimpossible without the ion engines.Xenon was chosen because it is chemically inert,easily stored in a compact form, and the atoms arerelatively heavy so they provide a relatively large thrustcompared to other candidate propellants. At launch,Dawn at Ceres11Press Kit

the gaseous xenon stored in the fuel tank was 1.5times the density of water.one camera is in use during normal operations,with the other held as a backup. Each camera isequipped with an f/7.9 refractive optical systemwith a focal length of 150 millimeters and can usea clear filter or seven color filters, provided mainlyto help study minerals on the surface of Vesta orCeres. In addition to detecting the visible light humans see, the cameras register near-infrared energy. The framing cameras were provided by theMax Planck Institute for Solar System Research,Gottingen, Germany, with significant contributionsby the German Aerospace Center (DLR) Instituteof Planetary Research, Berlin, and in coordination with the Institute of Computer and Communication Network Engineering, Braunschweig.The team lead for the framing camera, AndreasNathues, is based at the Max Planck Institute,Gottingen, Germany.At maximum thrust, each engine produces a total of91 millinewtons -- about the amount of force involvedin holding a single piece of notebook paper in yourhand.Solar PowerThe electrical power system provides power forall onboard systems, including the ion propulsionsystem when thrusting. Each of the two solar arraysis 27 feet (8.3 meters) long -- the width of a singlestennis court -- by 7.4 feet (2.3 meters) wide. From tipto tip, the spacecraft with fully deployed solar arrayswould extend from the pitcher’s mound to homeplate on a professional baseball field. On the frontside, 18 square meters (21.5 square yards) of eacharray is covered with 5,740 individual photovoltaiccells. The elemental composition of both Vesta and Ceres is measured with the gamma ray and neutron detector, or GRaND. This instrument usesa total of 21 sensors with a very wide field of viewto measure the energy from gamma rays andneutrons that either bounce off or are emitted bya celestial body. Gamma rays are a form of light,while neutrons are particles that normally residein the nuclei of atoms. Together, gamma rays andneutrons reveal many of the important atomicconstituents of the celestial body’s surface downto a depth of 3 feet (1 meter). Gamma rays andneutrons emanating from the surface of Vestaand Ceres can tell us much about the elementalcomposition of each. Many scientists believe thatCeres may be rich in water; if that is the case, thesignature of the water may be contained in thisinstrument’s data. Unlike the other instrumentsaboard Dawn, the detector has no internal datastorage. The instrument was built by Los AlamosNational Laboratory, Los Alamos, New Mexico.The team lead for the gamma ray and neutrondetector, Thomas Prettyman, is based at thePlanetary Science Institute, Tucson, Arizona. The surface mineralogy of both Vesta and Ceresis measured by the visible and infrared mapping spectrometer, or VIR. The instrument is amodification of a similar spectrometer on both theThe cells can convert about 28 percent of the solar energy that hits them into electricity. On Earth,the two wings combined could generate more than10,000 watts. The arrays are mounted on oppositesides of the spacecraft, with a gimbaled connectionthat allows them to be turned at any angle to face thesun.A nickel-hydrogen battery and associated chargingelectronics provided power during launch and continues to provide power at any time the solar arrays aredirected away from the sun.Science InstrumentsTo acquire science data at Vesta and Ceres, Dawncarries three instrument systems. In addition, anexperiment to measure gravity will be accomplishedwith existing spacecraft and ground systems. The framing camera is designed to acquiredetailed optical images for scientific purposes aswell as for navigation in the vicinities of Vesta andCeres. Dawn carries two identical and physicallyseparate cameras for redundancy, each withits own optics, electronics and structure. OnlyDawn at Ceres12Press Kit

European Space Agency’s Rosetta and Venus Express missions. It also draws significant heritagefrom the visible and infrared mapping spectrometer on NASA’s Cassini spacecraft. Each picturethe instrument takes records the light intensity atmore than 400 wavelength ranges in every pixel.When scientists compare its observations withlaboratory measurements of minerals, they candetermine what minerals are on the surfaces ofVesta and Ceres. The visible and infrared mappingspectrometer was funded and coordinated by theItalian Space Agency and built by SELEX ES, withthe scientific leadership of the Institute for SpaceAstrophysics and Planetology, Italian National Institute for Astrophysics, Italy. It is operated by theInstitute for Space Astrophysics and Planetology,Rome, Italy, led by Maria Cristina De Sanctis. As it did at Vesta, Dawn will make a set of scientific measurements at Ceres using the spacecraft’sradio transmitter and sensitive antennas on Earth.Monitoring signals from Dawn, scientists candet

Astrophysics and Planetology, Italian National Institute for Astrophysics, Italy, and is operated by the Institute for Space Astrophysics and Planetology, Rome, Italy. The gamma ray and neutron detector was built by Los Alamos National Laboratory, New Mexico, and is operated by the Plane

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