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Stardust (spacecraft)

Artist's rendering of Stardust-NExT performing a burn-to-depletion during the decommissioning of the spacecraft.
Operator NASA / JPL
Major contractors Lockheed Martin
Mission type Flyby, Sample return
Launch date 1999-02-07 21:04:15 UTC
Launch vehicle Delta II 7426
Launch site Cape Canaveral Air Force Station
Space Launch Complex 17A, Florida, U.S.
Mission duration 12 years, 1 month, 18 days
 Annefrank flyby
 (completed 2002-11-02)

 Wild 2 flyby
 (completed 2004-01-02)

 Sample return
 (completed 2006-01-15)

 Primary mission
 (completed 2006-01-15)

 Tempel 1 flyby
 (completed 2011-02-14)
Flyby of 5535 Annefrank, Wild 2, Tempel 1
Satellite of Sun
Landing site
Utah Test and Training Range
COSPAR ID 1999-003A
Homepage Stardust homepage
NExT homepage
Mass 300 kg (660 lb)
Power 330 W
(Solar array / NiH2 batteries)

Stardust was a 300-kilogram robotic space probe launched by NASA on February 7, 1999. Its primary mission was to collect dust samples from the coma of comet Wild 2, as well as samples of cosmic dust, and return these to Earth for analysis. It was the first sample return mission of its kind. En route to comet Wild 2, the craft also flew by and studied the asteroid 5535 Annefrank. The primary mission was successfully completed on January 15, 2006, when the sample return capsule returned to Earth.[1]

A mission extension codenamed NExT culminated in February 2011 with Stardust intercepting comet Tempel 1, a small Solar System body previously visited by Deep Impact in 2005. Stardust ceased operations in March 2011.

On August 14, 2014, scientists announced the identification of possible interstellar dust particles from the Stardust capsule returned to Earth in 2006.[2][3][4][5]


  • Mission background 1
    • History 1.1
    • Spacecraft design 1.2
      • Attitude control and propulsion 1.2.1
      • Communications 1.2.2
      • Power 1.2.3
      • Computer 1.2.4
      • Scientific instruments 1.2.5
      • Sample collection 1.2.6
    • Stardust microchip 1.3
  • Mission profile 2
    • Launch and trajectory 2.1
    • Encounter with Annefrank 2.2
    • Encounter with Wild 2 2.3
  • New Exploration of Tempel 1 (NExT) 3
    • Primary objectives 3.1
    • Encounter with Tempel 1 3.2
  • End of extended mission 4
  • Sample return 5
    • Sample processing 5.1
  • Results 6
  • See also 7
  • References 8
  • External links 9

Mission background


Beginning in the 1980s, scientists began seeking a dedicated mission to study a comet. During the early 1990s, several missions to study comet Halley became the first successful missions to return close-up data. However, the US cometary mission, Comet Rendezvous Asteroid Flyby, was canceled for budgetary reasons. In the mid-1990s, further support was given to a cheaper, Discovery-class mission that would study comet Wild 2 in 2004.[6]

Stardust was competitively selected in the fall of 1995 as a NASA Discovery Program mission of low-cost with highly focused science goals.[6]:5 Construction of Stardust began in 1996, and was subject to the maximum contamination restriction, level 5 nitrogen; indigenous aliphatic hydrocarbons with longer chain lengths than those observed in the diffuse interstellar medium; abundant amorphous silicates in addition to crystalline silicates such as olivine and pyroxene, proving consistency with the mixing of Solar System and interstellar matter, previously deduced spectroscopically from ground observations;[37] hydrous silicates and carbonate minerals were found to be absent, suggesting a lack of aqueous processing of the cometary dust; limited pure carbon (CHON) was also found in the samples returned; methylamine and ethylamine was found in the aerogel but was not associated with specific particles.

In 2010, Dr. Andrew Westphal announced that Stardust@home volunteer Bruce Hudson found a track (labeled "I1043,1,30") among the many images of the aerogel that may contain an interstellar dust grain.[38] The program allows for any volunteer discoveries to be recognized and named by the volunteer. Hudson named his discovery, Orion.[39]

In April 2011, scientists from the University of Arizona discovered evidence for the presence of liquid water in Comet Wild 2. They have found iron and copper sulfide minerals that must have formed in the presence of water. The discovery shatters the existing paradigm that comets never get warm enough to melt their icy bulk.[40] In the spring of 2014, the recovery of particles of interstellar dust from the Discovery program's Stardust mission was announced.[41]


The comet samples show that the outer regions of the early Solar System were not isolated and were not a refuge where interstellar materials could commonly survive.[42] The data suggest that high-temperature inner Solar System material formed and was subsequently transferred to the Kuiper Belt.[43]


In 2009 it was announced by NASA that scientists had identified one of the fundamental chemical building blocks of life in a comet for the first time: glycine, an amino acid, was detected in the material ejected from Comet Wild-2 in 2004 and grabbed by the Stardust probe. Glycine has been detected in meteorites before and there are also observations in interstellar gas clouds, but the Stardust find is described as a first in cometary material. Isotope analysis indicates that the Late Heavy Bombardment included cometary impacts after the Earth coalesced but before life evolved.[44] Carl Pilcher, who leads NASA's Astrobiology Institute commented that "The discovery of glycine in a comet supports the idea that the fundamental building blocks of life are prevalent in space, and strengthens the argument that life in the Universe may be common rather than rare."[45]

See also


  1. ^ Dolmetsch, Chris (2006-01-15). "NASA Spacecraft Returns With Comet Samples After 2.9 Bln Miles". Bloomberg. Archived from the original on 2013-03-28. 
  2. ^ Agle, DC; Brown, Dwayne; Jeffs, William (August 14, 2014). "Stardust Discovers Potential Interstellar Space Particles".  
  3. ^ Dunn, Marcia (August 14, 2014). "Specks returned from space may be alien visitors".  
  4. ^ Hand, Eric (August 14, 2014). "Seven grains of interstellar dust reveal their secrets".  
  5. ^ Westphal, A. J.; Stroud, R. M.; Bechtel, H. A.; Brenker, F. E.; et al. (2014). "Evidence for interstellar origin of seven dust particles collected by the Stardust spacecraft". Science 345 (6198): 786–791.  
  6. ^ a b c d e f g h i j k "Stardust Launch" (PDF) (Press release). NASA. 1999. Retrieved 2011-02-13. 
  7. ^ "Comets & The Question of Life". NASA. Retrieved 2008-03-04. 
  8. ^ a b c d e f g h i "STARDUST", STARDUST, NASA, 2006, retrieved 2011-02-14 
  9. ^ a b c d e "Stardust Flight System Description". NASA. Retrieved 2011-02-14. 
  10. ^ a b Newburn, R. L., Jr.; Bhaskaran, S.; Duxbury, T. C.; Fraschetti, G.; Radey, T.; Schwochert, M. (2003-10-14). "Stardust Imaging Camera". Journal of Geophysical Research 108 (8116).  
  11. ^ "Imaging and Navigation Camera". NASA / National Space Science Data Center. Retrieved 2011-02-19. 
  12. ^ a b Kissel, J; Glasmachers, A.; Grün, E.; Henkel, H.; Höfner, H.; Haerendel, G.; von Hoerner, H.; Hornung, K.; Jessberger, E. K.; Krueger, F. R.; Möhlmann, D.; Greenberg, J. M.; Langevin, Y.; Silén, J.; Brownlee, D.; Clark, B. C.; Hanner, M. S.; Hoerz, F.; Sandford, S.; Sekanina, Z.; Tsou, P.; Utterback, N. G.; Zolensky, M. E.; Heiss, C. (2003). "Cometary and Interstellar Dust Analyzer for comet Wild 2". Journal of Geophysical Research 108 (E10).  
  13. ^ "Cometary and Interstellar Dust Analyzer (CIDA)". NASA / National Space Science Data Center. Retrieved 2011-02-19. 
  14. ^ a b Tuzzolino, A. J. (2003). "Dust Flux Monitor Instrument for the Stardust mission to comet Wild 2". Journal of Geophysical Research 108 (E10).  
  15. ^ "Dust Flux Monitor Instrument (DFMI)". NASA / National Space Science Data Center. Retrieved 2011-02-19. 
  16. ^ a b Tsou, P.; Brownlee, D. E.; Sandford, S. A.; Horz, F.; Zolensky, M. E. (2003). "Wild 2 and interstellar sample collection and Earth return". Journal of Geophysical Research 108 (E10).  
  17. ^ "Stardust Sample Collection". NASA / National Space Science Data Center. Retrieved 2011-02-19. 
  18. ^ a b Anderson, John D.; Lau, Eunice L.; Bird, Michael K.; Clark, Benton C.; Giampieri, Giacomo; Patzold, Martin. "Dynamic science on the Stardust mission". Journal of Geophysical Research 108 (E10).  
  19. ^ "Dynamic Science". NASA / National Space Science Data Center. Retrieved 2011-02-19. 
  20. ^
  21. ^ "Stardust Put In Hibernation Mode". Archived from the original on 2006-01-31. 
  22. ^ a b "Stardust/NExT - Five Things About NASA's Valentine's Day Comet". NASA. 
  23. ^ "Mission Timeline" (Press release). NASA. 2011-02-14. 
  24. ^ Savage, Donald; Heil, Martha J. (2001-01-11). "Stardust can see clearly now - just before Earth flyby". JPL, NASA. Archived from the original on 2001-01-29. 
  25. ^ "Stardust Spacecraft Completes Comet Flyby". SpaceRef. 2011-02-15. 
  26. ^ Williams, David E. (2006-01-13). "Spacecraft bringing comet dust back to Earth". CNN. Archived from the original on 2006-01-27. 
  27. ^ "STARDUST". publisher=Extrasolar-Planets. Retrieved 2008-03-04. 
  28. ^ "Stardust-NExT" (PDF) (Press release). NASA. 2011. Archived from the original (PDF) on 2011-06-27. 
  29. ^ Segal, Kimberly; Zarrella, John (2011-02-16). "'"Crater on comet 'partly healed itself. CNN. Archived from the original on 2014-03-25. 
  30. ^ "NASA Stardust Spacecraft Officially Ends Operations". NASA Homepage: NASA. Retrieved 2011-04-10. The Stardust team performed the burn to depletion because the comet hunter was literally running on fumes. The depletion maneuver command was sent from the Stardust-NExT mission control area at Lockheed Martin Space Systems in Denver. The operation was designed to fire Stardust's rockets until no fuel remained in the tank or fuel lines. The spacecraft sent acknowledgment of its last command from approximately 312 million kilometers (194 million miles) away in space. 
  31. ^ a b "Stardust Reentry Simulation". YouTube user "Evelyn Parker". 2013-09-13.  Data in the simulation agrees with readings by the airborne observation team monitoring the reentry, available at "Stardust Capsule Reentry Movie". YouTube user "jotape". 2006-02-01. 
  32. ^ ReVelle, D. O.; Edwards, W. N. (2007). "Stardust—An artificial, low-velocity "meteor" fall and recovery: 15 January 2006" (PDF). The Meteoritical Society. 
  33. ^ Winter, Michael W.; Trumble, Kerry A. (2010). "Spectroscopic Observation of the Stardust Re-Entry in the Near UV with SLIT: Deduction of Surface Temperatures and Plasma Radiation" (PDF). NASA. 
  34. ^ "NASA's Comet Tale Draws to a Successful Close in Utah Desert". NASA. Retrieved 2008-03-04. 
  35. ^ "Stardust's Cargo Comes to Houston under Veil of Secrecy". Retrieved 2008-03-04. 
  36. ^ "The building blocks of planets within the 'terrestrial' region of protoplanetary disks". University of Nottingham. Retrieved 2008-03-04. 
  37. ^ Rincon, Paul (2010-03-05). "Probe may have found cosmic dust". BBC. 
  38. ^ Westphal, A. J.; Allen, C.; Bajt, S.; Bastien, R.; Bechtel, H.; Bleuet, P.; Borg, J.; Brenker, F.; Bridges, J.; et al. Analysis of "Midnight" Tracks in the Stardust Interstellar Dust Collector: Possible Discovery of a Contemporary Interstellar Dust Grain (PDF). 41st Lunar and Planetary Science Conference. 
  39. ^ LeBlanc, Cecile (2011-04-07). "Evidence for liquid water on the surface of Comet Wild-2". 
  40. ^ "Stardust Interstellar Dust Particles". JSC, NASA. 2014-03-13. Archived from the original on 2007-07-14. 
  41. ^ Brownlee, Don (2014-02-05). "The Stardust Mission: Analyzing Samples from the Edge of the Solar System". Annual Review of Earth and Planetary Sciences.  
  42. ^ Matzel, Jennifer E. P. (2010-04-23). "Constraints on the Formation Age of Cometary Material from the NASA Stardust Mission". Science 328 (5977): 483–486.  
  43. ^ Morbidelli, A.; Chambers, J.; Lunine, J. I.; Petit, J. M.; Robert, F.; Valsecchi, G. B.; Cyr, K. E. (February 2010). "Source regions and timescales for the delivery of water to the Earth". Meteoritics & Planetary Science 35 (6): 1309–1320.  
  44. ^ Life chemical' detected in comet"'". BBC News. 2009-08-18. 

External links

  • Stardust Project webpage
  • NASA Stardust mission page
  • Stardust Mission Profile by NASA's Solar System Exploration
  • Stardust@Home project - Volunteers needed
  • NASA video on the mission
  • Catalogue of raw images taken by Stardust
In December 2006, seven papers were published in the scientific journal,

The sample container was taken to a clean room with a cleanliness factor 100 times that of a hospital operating room to ensure the star and comet dust was not contaminated.[36] Preliminary estimations suggested at least a million microscopic specks of dust were embedded in the aerogel collector. Ten particles were found to be at least 100 micrometers (0.1 mm) and the largest approximately 1000 micrometers (1 mm). An estimated 45 interstellar dust impacts were also found on the sample collector, which reside on the back side of the cometary dust collector. Dust grains are being observed and analyzed by a volunteer team through the distributed computing project, Stardust@Home.

Visible dust grains in the aerogel collector
Visible dust grains in the aerogel collector.

Sample processing

News related to Stardust lands in Utah successfully at Wikinews

On January 16, 2006, at 05:57:00 UTC, the Sample Return Capsule successfully separated from Stardust and re-entered the Earth's atmosphere at 09:57:00 UTC, at a velocity of 12.9 km/s, the fastest reentry speed into Earth's atmosphere ever achieved by a man-made object. The capsule followed a drastic reentry profile, going from a velocity of Mach 36 to subsonic speed within 110 seconds.[32] Peak deceleration was 34 g,[33] encountered 40 seconds into the reentry at an altitude of 55 km over Spring Creek, Nevada.[32] The PICA heat shield reached a temperature of more than 2,900 °C during this steep reentry.[34] The capsule then parachuted to the ground, finally landing at 10:10:00 UTC at the Utah Test and Training Range (), near the U.S. Army Dugway Proving Ground.[35] The capsule was then transported by military aircraft from Utah to Ellington Air Force Base in Houston, Texas, then transferred by road to the Planetary Materials Curatorial facility at Johnson Space Center in Houston to begin analysis. NASA officials claimed "prudence" dictated that the materials be transferred in secrecy, though no security threats were apparent.[8]

the landing capsule as seen on the ground at the Utah Test and Training range
Landing capsule as seen by the recovery team.

Sample return

On March 24, 2011, Stardust conducted a burn to consume its remaining fuel. The spacecraft had little fuel left and scientists hoped the data collected would help in the development of a more accurate system for estimating fuel levels on spacecraft. After the data had been collected, no further antenna aiming was possible and the transmitter was switched off. The spacecraft sent an acknowledgement from approximately 312,000,000 kilometers (194,000,000 mi) away in space.[31]

End of extended mission

Tempel 1 from the Stardust-NExT spacecraft during closest approach.
Tempel 1 from the Stardust-NExT spacecraft during closest approach. 
'Before and after' comparison images from Deep Impact and Stardust, showing the crater formed by Deep Impact on the right hand image.
'Before and after' comparison images of Tempel 1 by Deep Impact (left) and Stardust (right). 

On February 15, 2011, at 04:42:00 UTC, Stardust-NExT encountered Tempel 1 from a distance of 181 km (112 mi). An estimated 72 images were acquired during the encounter. These showed changes in the terrain and revealed portions of the comet never seen by Deep Impact.[29] The impact site from Deep Impact was also observed, though it was barely visible due to material settling back into the crater.[30]

Encounter with Tempel 1

  • Potentially image and characterize the crater produced by Deep Impact in July 2005, to better understand the structure and mechanical properties of cometary nuclei and elucidate crater formation processes on them.
  • Measure the density and mass distribution of dust particles within the coma using the Dust Flux Monitor Instrument.
  • Analyze the composition of dust particles within the coma using the Comet and Interstellar Dust Analyzer instrument.

Secondary objectives

  • Extend the current understanding of the processes that affect the surfaces of comet nuclei by documenting the changes that have occurred on comet Tempel 1 between two successive perihelion passages, or orbits around the Sun.
  • Extend the geologic mapping of the nucleus of Tempel 1 to elucidate the extent and nature of layering, and help refine models of the formation and structure of comet nuclei.
  • Extend the study of smooth flow deposits, active areas and known exposure of water ice.

Primary objectives

The mission objectives included the following:[28]

On July 3, 2007 the mission extension was approved and renamed New Exploration of Tempel 1 (NExT). This investigation would provide the first look at the changes to a comet nucleus produced after a close approach to the Sun. NExT also would extend the mapping of Tempel 1, making it the most mapped comet nucleus to date. This mapping would help address the major questions of comet nucleus geology. The flyby mission was expected to consume almost all of the remaining fuel, signaling the end of the operability of the spacecraft.[22]

On March 19, 2006, Stardust scientists announced that they were considering the possibility of redirecting the spacecraft on a secondary mission to image Tempel 1. The comet was previously the target of the Deep Impact mission in 2005, sending an impactor into the surface. The possibility of this extension could be vital for gathering images of the impact crater Deep Impact was unsuccessful in capturing due to dust from the impact, obscuring the surface.

Mission logo

New Exploration of Tempel 1 (NExT)

Comet Wild 2 as seen from Stardust on January 2, 2004
Comet Wild 2 as seen from Stardust on January 2, 2004. 
Image of Wild 2 taken during the closest approach phase
Image of Wild 2 taken during the closest approach phase. 
An overexposed image of Wild 2 showing plumes of material coming from the surface
An overexposed image of Wild 2 showing plumes of material. 
A three-dimensional anaglyph of comet Wild 2
A 3D anaglyph of comet Wild 2 

During the flyby the spacecraft deployed the Sample Collection plate to collect dust grain samples from the coma, and took detailed pictures of the icy nucleus.[27]

The relative velocity between the comet and the spacecraft was such that the comet actually overtook the spacecraft from behind as they traveled around the Sun. During the encounter, the spacecraft was on the Sun-lit side of the nucleus, approaching at a solar phase angle of 70 degrees, reaching a minimum angle of 3 degrees near closest approach and departing at a phase angle of 110 degrees.[8]

On January 2, 2004, at 19:21:28 UTC, Stardust encountered Comet Wild 2[26] on the sunward side with a relative velocity of 6.1 km/s at a distance of 237 km (147 mi). The original encounter distance was planned to be 150 km (93 mi), but this was changed after a safety review board increased the closest approach distance to minimize the potential for catastrophic dust collisions.[8]

Encounter with Wild 2

Image of asteroid Annefrank captured on November 2, 2002
Image of asteroid Annefrank captured on November 2, 2002. 
A false-color image of asteroid Annefrank showing the irregular shape of the small solar system body
False-color image of asteroid Annefrank 

On November 2, 2002, at 04:50:20 UTC, Stardust encountered asteroid 5535 Annefrank from a distance of 3,079 km (1,913 mi). The solar phase angle ranged from 130 deg to 47 degrees during the period of observations. This encounter was used primarily as an engineering test of the spacecraft and ground operations in preparation for the encounter with comet Wild 2 in 2003.[8]

Encounter with Annefrank

Exploded diagram of the Delta II vehicle with Stardust
Exploded diagram of the Delta II vehicle with Stardust
Photo of Stardust during launch with a Delta II launch vehicle
Stardust during launch with a Delta II launch vehicle. 
Trajectory of the Stardust spacecraft
Trajectory of the Stardust spacecraft en route to Wild 2. 
Timeline of travel[8][23]
Date Event
Spacecraft launched at 21:04:15 UTC
Stardust Sample Collection test.
Earth gravity assist maneuver
New record in spaceflight set: furthest solar powered object at 2.72 AU.
Flyby encounter with Annefrank
Flyby encounter with Wild 2
Earth return of sample capsule.
Flyby encounter with Tempel 1.
End of mission.

A subsequent mission extension was approved on July 3, 2007, to bring the spacecraft back to full operation for a flyby of comet Tempel 1 in 2011. The mission extension was the first to revisit a small Solar System body and used the remaining propellant, signaling the end of the useful life for the spacecraft.[22]

On January 29, 2004, the spacecraft was put in hibernation mode with only the solar panels and receiver active, in a three-year heliocentric orbit that would return it to Earth vicinity on January 14, 2009.[8][21]

During the second encounter with Earth, Stardust was put into a "divert maneuver" immediately after the capsule was released. The maneuver corrected the spacecraft direction to avoid entering the atmosphere. Under twenty kilograms of propellant remained onboard after the maneuver.[8]

Stardust was launched on February 7, 1999, at 21:04:15 UTC by the National Aeronautics and Space Administration from Space Launch Complex 17A at the Cape Canaveral Air Force Station in Florida, aboard a Delta II 7426 launch vehicle. The complete burn sequence lasted for 27 minutes bringing the spacecraft into a heliocentric orbit that would bring the spacecraft around the Sun and past Earth for a gravity assist maneuver in 2001, to reach asteroid Annefrank in 2002 and comet Wild 2 in 2004 at a low flyby velocity of 6.1 km/s. In 2004, the spacecraft performed a course correction that would allow it to pass by Earth a second time in 2006, to release the Sample Return Capsule for a landing in Utah in the Bonneville Salt Flats.[6]:14–22[8]

Launch and trajectory

Mission profile

Stardust was launched carrying two sets of identical pairs of square 10.16-centimeter (4.00 in) silicon wafers. Each pair featured engravings of well over one million names of people who participated in the public outreach program by filling out internet forms available in late 1997 and mid-1998. One pair of the microchips was positioned on the spacecraft and the other was attached to the sample return capsule.[6]:24

Stardust microchip

Images of the spacecraft
Diagram of the spacecraft
Diagram of the spacecraft. 
Stardust capsule with aerogel collector deployed
Stardust capsule with aerogel collector deployed 
Stardust awaiting testing of the solar arrays
Stardust awaiting testing of the solar arrays. 
The solar arrays being checked in the Payload Hazardous Servicing Facility
The solar arrays being checked in the Payload Hazardous Servicing Facility. 
Stardust being checked before encapsulation
Stardust being checked before encapsulation. 

To analyze the aerogel for interstellar dust, one million photographs will be needed to image the entirety of the sampled grains. The images will be distributed to home computer users to aid in the study of the data using a program titled, Stardust@home. In April 2014, NASA reported they had recovered seven particles of interstellar dust from the aerogel.[20]

To collect the particles without damaging them, a silicon-based solid with a porous, sponge-like structure is used in which 99.8 percent of the volume is empty space. Aerogel has 1/1000th the density of glass, another silicon-based solid to which it may be compared. When a particle hits the aerogel, it becomes buried in the material, creating a long track, up to 200 times the length of the grain. The aerogel was packed in an aluminium grid and fitted into a Sample Return Capsule (SRC), which was to be released from the spacecraft as it passed Earth in 2006.

Comet and interstellar particles are collected in ultra low density aerogel. The tennis racket-sized collector tray contains ninety blocks of aerogel, providing more than 1,000 square centimeters of surface area to capture cometary and interstellar dust grains.

Sample collection

Navigation Camera (NC)
The camera is intended for targeting comet Wild 2 during the flyby of the nucleus. It captures black and white images through a filter wheel making it possible to assemble color images and detect certain gas and dust emissions in the coma. It also captures images at various phase angles, making it possible to create a three-dimensional model of a target to better understand the origin, morphology, and mineralogical inhomogeneities on the surface of the nucleus. The camera utilizes the optical assembly from the Voyager Wide Angle Camera. It is additionally fitted with a scanning mirror to vary the viewing angle and avoid potentially damaging particles. For environmental testing and verification of the NAVCAM the only remaining Voyager spare camera assembly was used as a collimator for testing of the primary imaging optics. A target at the focal point of the spare was imaged through the optical path of the NAVCAM for verification.[10][11]
  • Lead investigator: Ray Newburn / JPL
  • Data: PDS/SBN data catalog
Cometary and Interstellar Dust Analyzer (CIDA)
The dust analyzer is a mass spectrometer able to provide real-time detection and analysis of certain compounds and elements. Particles enter the instrument after colliding with a silver impact plate and traveling down a tube to the detector. The detector is then able to detect the mass of separate ions by measuring the time taken for each ion to enter and travel through the instrument. Identical instruments were also included on Giotto and Vega 1 and 2.[12][13]
  • Lead investigator: Jochen Kissel / Max-Planck-Institut fur Aeronomie (website -archived)
  • Data: PDS/SBN data archives: Early calib, Annefrank, Raw Wild 2, Calib Wild 2
Dust Flux Monitor Instrument (DFMI)
Located on the whipple shield at the front of the spacecraft, the sensor unit provides data regarding the flux and size distribution of particles in the environment around Wild 2. It records data by generating electric pulses as a special polarized plastic (PVDF) sensor is struck by high energy particles as small as a few micrometers.[14][15]
  • Lead investigator: Anthony Tuzzolino / University of Chicago (website)
  • Data: PDS/SBN data archive, PDS/SBN EDR data archive
Stardust Sample Collection (SSC)
The particle collector uses aerogel, a low-density, inert, microporous, silica-based substance, to capture dust grains as the spacecraft passes through the coma of Wild 2. After sample collection was complete, the collector receded into the Sample Return Capsule for entering the Earth's atmosphere. The capsule with encased samples would be retrieved from Earth's surface and studied.[16][17]
  • Principal investigator: Donald Brownlee / University of Washington
  • Data: PDS/SBN temperature data archive, PDS/SBN positioning data archive
Dynamic Science Experiment (DSE)
The experiment will primarily utilize the X band telecommunications system to conduct radio science on Wild 2, to determine the mass of the comet; secondarily the inertial measurement unit is utilized to estimate the impact of large particle collisions on the spacecraft.[18][19]
  • Lead investigator: John Anderson / JPL
  • Data: PDS/SBN data archive

Scientific instruments

The computer on the spacecraft operated using a radiation hardened RAD6000 32-bit processor card. For storing data when the spacecraft was unable to communicate with Earth, the processor card was able to store 128-megabytes, 20% of which was occupied by the flight system software. The system software is a form of VxWorks, an embedded operating system developed by Wind River Systems.[6]:31[9]


The probe was powered by two solar arrays, providing an average of 330 watts of power. The arrays also included whipple shields to protect the delicate surfaces from the potentially damaging cometary dust while the spacecraft was in the coma of Wild 2. The solar array design was derived primarily from the Small Spacecraft Technology Initiative (SSTI) spacecraft development guidelines. The arrays provided a unique method of switching strings from series to parallel depending on the distance from the Sun. A single nickel hydrogen (NiH2) battery was also included to provide the spacecraft with power when the solar arrays received too little sunlight.[6]:31[9]


For communicating with the Deep Space Network, the spacecraft transmitted data across the x-band using a 0.6-meter (2 ft 0 in) parabolic high-gain antenna, medium-gain antenna (MGA) and low-gain antennas (LGA) depending on mission phase, and a 15-watt transponder design originally intended for the Cassini spacecraft.[6]:32[9]


The spacecraft was three-axis stabilized with eight 4.41-N hydrazine monopropellant thrusters, and eight 1-N thrusters to maintain attitude control; necessary minor propulsion maneuvers were performed by these thrusters as well. The spacecraft was launched with 80-kilograms of propellant. Information for spacecraft positioning was provided by a star camera using FSW to determine attitude (stellar compass), an inertial measurement unit, and two sun sensors.[6]:30–31[9]

Attitude control and propulsion

The spacecraft bus measured 1.7 meters (5.6 ft) in length, and 0.66 meters (2.2 ft) in width, a design adapted from the SpaceProbe deep space bus developed by Lockheed Martin Astronautics. The bus was primarily constructed with graphite fiber panels with an aluminum honeycomb support structure underneath; the entire spacecraft was covered with polycyanate, Kapton sheeting for further protection. To maintain low costs, the spacecraft incorporated many designs and technologies used in past missions or previously developed for future missions by the Small Spacecraft Technologies Initiative (SSTI). The spacecraft featured five scientific instruments to collect data, including the Stardust Sample Collection tray, which was brought back to Earth for analysis.[9]

Spacecraft design

The spacecraft was designed, built and operated by Lockheed Martin Astronautics as a Discovery-class mission in Denver, Colorado. JPL provided mission management for the NASA division for mission operations. The principal investigator of the mission was Dr. Donald Brownlee from the University of Washington.[6]:5

  • Providing a flyby of a comet of interest (Wild 2) at a sufficiently low velocity (less than 6.5 km/s) such that non-destructive capture of comet dust is possible using an aerogel collector.
  • Facilitating the intercept of significant numbers of interstellar dust particles using the same collection medium, also at as low a velocity as possible.
  • Returning as many high resolution images of the comet coma and nucleus as possible, subject to the cost constraints of the mission.

The primary science objectives of the mission included:[8]

Comet Wild 2 was selected as the primary target of the mission for the rare chance to observe a long-period comet that has ventured close to the Sun. The comet has since become a short period comet after an event in 1974, where the orbit of Wild 2 was affected by the gravitational pull of Jupiter, moving the orbit inward, closer to the Sun. In planning the mission, it was expected that most of the original material from which the comet formed would still be preserved.[6]:5


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