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Let us define the TCM abbreviation here, which is used below, rather than the TCM1 abbreviation, which is not used, so it should not be defined.
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== Status ==
== Status ==
After initial checkout, during which the [[ion thrusters]] accumulated more than 11 days of thrust, ''Dawn'' began long-term cruise propulsion on
After initial checkout, during which the [[ion thrusters]] accumulated more than 11 days of thrust, ''Dawn'' began long-term cruise propulsion on
December 17, 2007.<ref>{{cite web | url = http://dawn.jpl.nasa.gov/mission/journal_12_17_07.asp | title = Dawn Journal: December 17, 2007 | last = Rayman | first = Marc D. | publisher = JPL}}</ref> On October 31, 2008, ''Dawn'' completed its first thrusting phase to send it on to Mars for a [[gravity assist]] flyby in February 2009. During this first interplanetary cruise phase ''Dawn'' has spent 270 days, or 85% of this phase using its thrusters. It has expended less than 72 kilograms (158 pounds) of [[Xenon]] [[propellant]] for a total change in velocity of 1.81 kilometers per second (4050 miles per hour). On November 20, 2008, ''Dawn'' performed its first [[trajectory]] correction maneuver (TCM1), firing its #1 thruster for 2 hours, 11 minutes. The next scheduled TCM is January 2009 following [[Conjunction (astronomy and astrology)|solar conjunction]] on December 12, 2008 and prior to closest approach to Mars on February 17, 2009.<ref>[http://www.planetary.org/blog/article/00001755/ Dawn Journal: Aiming away from a bull's eye at Mars]</ref>
December 17, 2007.<ref>{{cite web | url = http://dawn.jpl.nasa.gov/mission/journal_12_17_07.asp | title = Dawn Journal: December 17, 2007 | last = Rayman | first = Marc D. | publisher = JPL}}</ref> On October 31, 2008, ''Dawn'' completed its first thrusting phase to send it on to Mars for a [[gravity assist]] flyby in February 2009. During this first interplanetary cruise phase ''Dawn'' has spent 270 days, or 85% of this phase using its thrusters. It has expended less than 72 kilograms (158 pounds) of [[Xenon]] [[propellant]] for a total change in velocity of 1.81 kilometers per second (4050 miles per hour). On November 20, 2008, ''Dawn'' performed its first [[trajectory]] correction maneuver (TCM), firing its #1 thruster for 2 hours, 11 minutes. The next scheduled TCM is January 2009 following [[Conjunction (astronomy and astrology)|solar conjunction]] on December 12, 2008 and prior to closest approach to Mars on February 17, 2009.<ref>[http://www.planetary.org/blog/article/00001755/ Dawn Journal: Aiming away from a bull's eye at Mars]</ref>


==Mission==
==Mission==

Revision as of 18:17, 4 January 2009

Template:Infobox Spacecraft Dawn, launched on September 27, 2007, is a robotic spacecraft being sent by NASA on a space exploration mission to the two most massive members of the asteroid belt: the asteroid Vesta and the dwarf planet Ceres. Dawn is scheduled to explore Vesta between 2011 and 2012, and Ceres in 2015. It will be the first spacecraft to visit either body.

Dawn is innovative in that it will be the first spacecraft to enter into orbit around a celestial body, study it, and then re-embark under powered flight to proceed to a second target. All previous multi-target study missions—such as the Voyager program—have involved rapid planetary flybys.

Launch

Dawn was scheduled to launch from pad 17-B at the Cape Canaveral Air Force Station on a Delta 7925-H rocket.[1] On April 10, 2007, Dawn arrived at the Astrotech Space Operations subsidiary of SPACEHAB, Inc. in Titusville, Florida, where it was prepared for launch.[2][3] Launch was originally scheduled for June 20, but was delayed until June 30 due to delays with part deliveries.[4] A broken crane at the launch pad, used to raise the solid rocket boosters, delayed the launch for a week, until July 7, but on June 15 the second stage was successfully hoisted into position.[5][6] A mishap at the Astrotech Space Operations facility, involving slight damage to one of the solar arrays, did not have an effect on the launch date, however bad weather caused the launch to slip to July 8. Range tracking problems then delayed the launch to July 9, and then July 15, before the launch was delayed further to avoid knock-on delays with the Phoenix mission to Mars, which was successfully launched on August 4.

A Delta II launching Dawn from CCAFS LC-17

Launch of Dawn was then rescheduled for September 26, 2007.[7][8] However the launch was then delayed to September 27, due to bad weather delaying fuelling of the second stage, the same problem which had earlier delayed the July 7 launch attempt. The launch window extended from 7:20 a.m. - 7:49 a.m. EDT (11:20 - 11:49 GMT).[9] During the final built-in hold at T-4 minutes, a ship entered the exclusion area offshore, the sea strip where the rocket boosters are likely to fall after separation. The ship was commanded to leave the area, then the launch had to wait for the end of a collision avoidance window with the ISS.[10] The spacecraft finally launched at 7:34 a.m. EDT from pad 17-B on a Delta II launch vehicle.[11][12][13]

The launch rocket propelled Dawn to 11.46 kilometers per second (25,600 miles per hour) relative to earth.[14] Thereafter Dawn's ion thrusters took over.

Status

After initial checkout, during which the ion thrusters accumulated more than 11 days of thrust, Dawn began long-term cruise propulsion on December 17, 2007.[15] On October 31, 2008, Dawn completed its first thrusting phase to send it on to Mars for a gravity assist flyby in February 2009. During this first interplanetary cruise phase Dawn has spent 270 days, or 85% of this phase using its thrusters. It has expended less than 72 kilograms (158 pounds) of Xenon propellant for a total change in velocity of 1.81 kilometers per second (4050 miles per hour). On November 20, 2008, Dawn performed its first trajectory correction maneuver (TCM), firing its #1 thruster for 2 hours, 11 minutes. The next scheduled TCM is January 2009 following solar conjunction on December 12, 2008 and prior to closest approach to Mars on February 17, 2009.[16]

Mission

The mission's goal is to characterise the conditions and processes of the solar system's earliest epoch by investigating in detail two of the largest protoplanets remaining intact since their formation. Ceres and Vesta have many contrasting characteristics that are thought to have resulted from them forming in two different regions of the early solar system; Ceres is theorized to have experienced a "cool and wet" formation that may have left it with subsurface water, and Vesta is theorised to have experienced a "hot and dry" formation that resulted in a differentiated interior and surface volcanism.

Using a framing camera along with two redundant cameras,[17] a visual and infared spectrometer, and a Gamma Ray and Neutron Spectrometer,[18] Dawn will take pictures and measure the chemical composition of Ceres and Vesta.[19]

To cruise from Earth to its targets it will travel in a long outward spiral. The current estimated chronology is as follows:[20]

Planned flight trajectory
  • September 27, 2007: launch
  • February 2009: Mars gravity assist
  • September 2011: Vesta arrival
  • April 2012: Vesta departure
  • February 2015: Ceres arrival
  • July 2015: End of operations

NASA posts the current location of Dawn on the web.[21]

An extended mission in which Dawn explores other asteroids after Ceres is also possible, although unlikely, as greater return is expected by spending the available time at Vesta and Ceres.[22]

Mission team

The Dawn mission team is led by UCLA space scientist and Dawn Principal Investigator Christopher T. Russell. Michael Mook is the Dawn Program Manager at Orbital Sciences Corporation, which built the spacecraft. Armando Piloto is the Dawn Mission Manager at Kennedy Space Center. NASA's Jet Propulsion Laboratory provided the Ion Propulsion System and management of the overall flight system development. The German Aerospace Center (DLR) and the Max Planck Institute for Solar System Research provided the framing camera, the Italian Space Agency provided the mapping spectrometer, and the DOE Los Alamos National Laboratory provided the gamma ray and neutron spectrometer.[23]

Motivation

Dawn waits for encapsulation at its launch pad on July 1, 2007

Dawn is intended to study two large bodies in the asteroid belt in order to answer questions about the formation of the solar system.

Ceres and Vesta were chosen as two contrasting protoplanets, one apparently "wet" (that is, icy) and the other "dry" (or rocky), whose accretion was terminated by the formation of Jupiter. They provide a bridge in our understanding between the formation of rocky planets and the icy bodies of our solar system, and under what conditions a rocky planet can hold water.

The IAU adopted a new definition of planet on August 24, 2006, and thus, if the IAU's definition stands and the spacecraft experiences no delays, Dawn will become the first mission to study a dwarf planet, arriving at Ceres five months prior to the arrival of New Horizons at Pluto.

Ceres is a dwarf planet whose mass comprises about one-third of the total mass of the bodies in the asteroid belt and whose spectral characteristics suggest a composition similar to that of a water-rich carbonaceous chondrite. Smaller Vesta, a water-poor achondritic asteroid, has experienced significant heating and differentiation. It shows signs of a metallic core, a Mars-like density and lunar-like basaltic flows.

Both bodies formed very early in the history of the solar system, thereby retaining a record of events and processes from the time of the formation of the terrestrial planets. Radionuclide dating of pieces of meteorites thought to come from Vesta suggests that Vesta differentiated quickly, in only three million years. Thermal evolution studies suggest that Ceres must have formed a little later, more than three million years after the formation of CAIs (the oldest known objects of Solar System origin).

Moreover, Vesta is the source of many smaller objects in the solar system. Most (but not all) V-type near-Earth asteroids, and some outer main-belt asteroids have spectra similar to Vesta and are known as 'vestoids'. Five percent of the found meteoritic samples on Earth, the Howardite Eucrite Diogenite ("HED") meteorites, are thought to be the result of a collision or collisions with Vesta.

Mission cancellations and reinstatements

The slightly damaged solar array (NASA)

The status of the Dawn mission has changed several times. In December 2003, the project was first cancelled,[24] and then reinstated in February 2004. In October 2005, work on Dawn was placed into "stand down" mode. In January 2006, Dawn's "stand down" was discussed in the press as "indefinitely postponed", even though NASA had announced no new decisions regarding the mission's status.[25] On March 2, 2006, Dawn was publicly, but not formally cancelled by NASA headquarters.[26]

However, the spacecraft's manufacturer Orbital Sciences Corporation appealed the decision and offered to build the spacecraft at cost, forgoing any profit in order to gain experience in a new market field. NASA then put the cancellation under review,[27] and on March 27, 2006, it was announced that the mission would not be cancelled after all.[28][29] In the last week of September 2006, the Dawn mission instrument payload integration reached a full functional status.

Propulsion system

The Dawn spacecraft is propelled by three DS1 heritage xenon ion thrusters (firing only one at a time). They have a specific impulse of 3100 s and produce a thrust of 90 mN.[30] The whole spacecraft, including the ion propulsion thrusters, is powered by a 10 kW triple-junction photovoltaic solar array.[31] To get to Vesta, Dawn will use Template:Kg to lb Xe and another Template:Kg to lb to get to Ceres,[32] out of a total of 425 kg (937 pounds) of on-board propellant.[33] All in all, it will perform a velocity change of over 10 km/s, far more than any other spacecraft has done.[32] Dawn is NASA’s first purely exploratory mission to use ion propulsion engines.[34]

The Dawn microchip

Onboard Dawn is a small computer microchip bearing the names of more than 360,000 space enthusiasts.[35] The names were submitted online as part of a public outreach effort between September 2005 and November 4, 2006.[36] The microchip (about the size of a nickel) was installed above the forward ion thruster, underneath the spacecraft's High Gain Antenna, on May 17, 2007.[37] More than one microchip was made, with a back-up copy on display at the 2007 Open House at the Jet Propulsion Laboratory in Pasadena, California.

References and notes

  1. ^ "Expendable Launch Vehicle Status Report". NASA. 2007-05-11.
  2. ^ NASA. "Dawn arrives in Florida". Spaceflight Now.
  3. ^ "Dawn at Astrotech's Payload Processing Facility". Space and Astronautics News.
  4. ^ "Launch of Dawn asteroid mission postponed again". NewScientistSpace.
  5. ^ "Pad 17 crane to be fixed mid-week". Florida Today.
  6. ^ "Expendable Launch Vehicle Status Report". June 18, 2007. {{cite web}}: Check date values in: |date= (help)
  7. ^ "NASA Mission to Asteroid Belt Rescheduled for September Launch". NASA. July 7, 2007. {{cite web}}: Check date values in: |date= (help)
  8. ^ "Dawn Launch Date". NASA launch schedule. Retrieved 2007-09-01.
  9. ^ "Expendable Launch Vehicle Status Report". NASA. September 7 2007. {{cite web}}: Check date values in: |date= (help)
  10. ^ "NASA's Launch Blog". NASA. September 27, 2007. {{cite web}}: Check date values in: |date= (help)
  11. ^ "ULA—One Team for Assured Access to Space" (PDF). ulalaunch.com. Retrieved 2008-03-04.
  12. ^ "NASA's Launch Coverage". NASA. September 27, 2007. {{cite web}}: Check date values in: |date= (help)
  13. ^ "Dawn Spacecraft Successfully Launched". NASA.
  14. ^ http://www-ssc.igpp.ucla.edu/dawn/DawnJournal_24August08.html
  15. ^ Rayman, Marc D. "Dawn Journal: December 17, 2007". JPL.
  16. ^ Dawn Journal: Aiming away from a bull's eye at Mars
  17. ^ Framing Camera for Dawn
  18. ^ Science Payload
  19. ^ GRaND science instrument moves closer to launch from Cape
  20. ^ GSpace Topics: Dawn
  21. ^ http://neo.jpl.nasa.gov/orbits/fulltraj.jpg
  22. ^ "Frequently asked questions". NASA. Retrieved 2008-07-14. {{cite web}}: Italic or bold markup not allowed in: |publisher= (help)
  23. ^ Rayman M. D., Fraschetti T. C., Raymond C. A., Russell C. T. (2006). "Dawn: A mission in development for exploration of main belt asteroids Vesta and Ceres". Acta Astronautica. 58 (11): 605–616. doi:10.1016/j.actaastro.2006.01.014.{{cite journal}}: CS1 maint: multiple names: authors list (link)
  24. ^ Ambrosiano, Nancy (2006-03-28). "NASA's Dawn mission is a go". Los Alamos National Laboratory. Retrieved 2007-10-01.
  25. ^ Chang, Alicia (2006). "NASA Asteroid Mission Won't Launch This Year". Space.com. Retrieved 2006-03-04.
  26. ^ Clark, Stephen (2006). "Probe built to visit asteroids killed in budget snarl". Spaceflightnow.com. Retrieved 2006-03-04.
  27. ^ "NASA reviewing canceled mission". CNN.com. March 16, 2006. Retrieved 2006-03-27.
  28. ^ Geveden, Rex (2006). "Dawn Mission Reclama" (PDF). Retrieved 2006-03-27.
  29. ^ Malik, Tariq (27 March 2006). "NASA Reinstates Cancelled Asteroid Mission". Space.com. Retrieved 2006-03-27. {{cite web}}: Check date values in: |date= (help)
  30. ^ "Dawn, Ion Propulsion". NASA. Retrieved 2007-09-28.
  31. ^ "Dawn, Spacecraft". NASA. Retrieved 2007-09-28.
  32. ^ a b "Dawn: Mission description". UCLA Space Physics Center. 2006-10-17. Retrieved 2007-09-28.
  33. ^ Watanabe, Susan (2007-07-05). "Dawn: Spacecraft & Instruments". NASA. Retrieved 2006-08-10.
  34. ^ "Dawn Lifts Off". National Geographic Society. Retrieved 2007-09-28.
  35. ^ "All Aboard the Dawn Spacecraft". JPL.NASA.gov. May 20, 2007. Retrieved 2007-06-21.
  36. ^ "Send Your Name to the Asteroid Belt". JPL.NASA.gov. November 4, 2006. Retrieved 2007-06-21.
  37. ^ "Kennedy Media Gallery". KSC.NASA.gov. May 17, 2007. Retrieved 2007-06-21.

See also

Media related to Dawn (spacecraft) at Wikimedia Commons


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