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       CONTOUR Tour
                                      Sun
                           Earth
Sc
     hw
         Comet Nucleus
       ass
          man
             n–Wachmann
                        3
                                                  A Mission to Study the Diversity of Comet Nuclei

       The CONTOUR mission is our most detailed                         MISSION PROFILE
       look yet at the heart of a comet — its nucleus.                  • Launch: July 2002 from Cape Canaveral Air Force
       CONTOUR will fly to within 100 kilometers (about                   Station, Florida, aboard a Delta II (7425) launch vehicle.
       60 miles) of at least two comet nuclei, assessing
       their diversity and discovering how these primitive              • Innovative Launch Concept: CONTOUR orbits
       building blocks of the solar system have evolved                   Earth for several weeks after launch, moving into
                                                                          position for maneuver sending it into a solar orbit
       since forming more than 4.5 billion years ago.
                                                                          on Aug. 15, 2002.
          Key Measurements
                                                                        • Close-up Encounters: Fly past and collect data on
          • Detailed imaging of the nucleus                               comets Encke (Nov. 2003) and Schwassmann-
             (4-meter resolution)                                         Wachmann 3 (June 2006).
          • Spectral mapping of the nucleus
             (100- to 200-meter resolution)                             • Mission Flexibility: Earth swingbys (gravity-assist
          • Analysis of gas and dust surrounding                          maneuvers) refine trajectory for comet encounters
                                                                          or retarget spacecraft toward a “new” comet.
             the nucleus
                                                                           — Swingbys occur Aug. 2003; Aug. 2004;
       THE SPACECRAFT                                                          Feb. 2005; Feb. 2006.
       Simple and compact, CONTOUR has few hinged and                   • Minimal Operations Support: Spacecraft
       movable parts; a body-mounted solar array; and a                   spends 65% of flight in unattended, spin-stabilized
       mission geometry suitable for fixed, passive antennas.             “hibernation.”
       Operators point the instruments and antennas by moving
       the spacecraft. A layered shield of Nextel and Kevlar
       protects CONTOUR from speeding dust and particles                           CONTOUR Remote Imager/Spectrograph (CRISP)
                                                                                     • Takes high-resolution photos of nucleus
       near the nucleus.
                                                                                     • Maps ice and rock types on surface
       • 8-sided body; 2 meters (6 feet) tall; 2 meters wide                           Mass: 26.7 kg (59 pounds)
       • Total weight: 970 kilograms (2,138 pounds)                                    Power: 45 watts (average)
         — Dry spacecraft: 387 kilograms                                               Supplier: Johns Hopkins University
                                                                                       Applied Physics Laboratory
         — Solid rocket motor: 503 kilograms
         — Hydrazine fuel: 80 kilograms                                                                         Dust Shield
       • Two modes of operation
         — Spin-stabilized cruise mode                                                         Neutral Gas and Ion Mass Spectrometer
         — Precision, 3-axis stabilized                                                        (NGIMS)
             encounter mode                                                                       • Counts and analyzes atoms,
                                                                                                    molecules and ions around nucleus
       • Designed for solar distance                                                                Mass: 13.5 kg (30 pounds)
         up to 195 million kilometers                                                               Power: 47 watts (average)
         (about 121 million miles).                                                                 Supplier: NASA/
       • Two, 5-gigabit solid-                                                                      Goddard Space Flight Center
         state data recorders
                                                                                                 Comet Impact Dust Analyzer (CIDA)
          Thruster Pods                                                                            • Determines composition of
          (2 of 4)                                                                                   dust surrounding nucleus
                                                                                                     Mass: 10.5 kg (23 pounds)
       CONTOUR Forward Imager (CFI)                                                                  Power: 13 watts (average)
         • Locates comet on approach                                                                 Supplier: von Hoerner
         • Snaps color pictures of gas, dust jets near nucleus                                       & Sulger, GmbH
           Mass: 9.7 kg (21 pounds)
           Power: 10 watts (average)
           Supplier: Johns Hopkins University
           Applied Physics Laboratory
THE COMETS                                                                                    THE ENCOUNTERS
CONTOUR’s target comets have                                                                  CONTOUR first “sees” the target
diverse physical characteristics and will                                                     comet several days before each
be relatively close to Earth during each                                                      encounter, while the nucleus is still
encounter.                                                                                    thousands of kilometers away. The
Evolved yet active, Encke has been                                                            mission team then directs the craft
observed at more apparitions (57)                                                             toward the comet and prepares to
than any other comet, even Halley.                                                            gather data.
Encke takes about 3 years to orbit the                                                           Timeline
Sun. Encke has traveled this orbit for                      48 seconds (1,350 kilometers)        60 to 10 days before encounter:
thousands of years, so its continued                                                             The mission team determines the
activity is rather puzzling.                                                                     spacecraft’s position and checks out
Schwassmann-Wachmann 3 was                                                                       its systems and instruments.
discovered in 1930. Its activity was                                                             10 days to 12 hours before:
predictable until the mid-1990s, when                                                            CONTOUR snaps pictures and makes
it split into several pieces. When                                                               spectral observations of the coma. The
CONTOUR reaches SW3 in 2006,                                                                     images also help operators navigate the
it could see relatively fresh, unaltered                                                         spacecraft.
surfaces and evidence of materials inside                                                        12 hours before to 12 hours after:
the nucleus.                                                                                     CONTOUR is in full encounter mode;
                                                            20 seconds (475 kilometers)          all instruments are turned on and
      A “New” Comet
                                                                                                 programmed to fill the spacecraft’s
      Should a new, scientifically
                                                                                                 data recorders.
      appealing comet reach the inner
      solar system during the mission,                                                           12 hours to 15 days after:
                                                                                                 CONTOUR sends data back to Earth,
      CONTOUR can change its path
                                                                                                 and the mission team verifies the
      (after the Encke encounter) to
                                                                                                 spacecraft’s orbit.
      study it. The potential target
      should be active and bright —
      much like comet Hale-Bopp,                                                             THE CAMERA EYE
      which was prominent in 1997.                                                           A simulated look at Encke’s nucleus
                                                                                             through CRISP, noting time and
                                                             8 seconds (260 kilometers)
1 astronomical unit (AU) is the average distance                                             distance to closest approach.
between Earth and the Sun, about 150 million kilometers
(93 million miles).

                                  Sun             Earth         Flyby      A NASA DISCOVERY MISSION
        Encounter               Distance         Distance      Speed       CONTOUR is the sixth mission in NASA’s innovative
          Date                    (AU)             (AU)       (km/sec)     Discovery Program of low-cost, highly focused scientific
    Encke, 11/12/03                1.08            0.27         28.2       exploration projects. Other Discovery missions to small
                                                                           bodies include Near Earth Asteroid Rendezvous (NEAR)
      SW3, 6/19/06                 0.96            0.32         14.0
                                                                           — the first mission to orbit and land on an asteroid — the
                                                                           Stardust and Deep Impact comet studies, and the Dawn
MISSION MANAGEMENT                                                         asteroid-orbiter mission. For more information visit
Principal Investigator:                                                    http://discovery.nasa.gov.
Dr. Joseph Veverka, Cornell University
Project Management, Spacecraft Development                                 EDUCATION AND PUBLIC OUTREACH
and Mission Operations:                                                    The mission’s comprehensive Education and Public
The Johns Hopkins University                                               Outreach efforts are designed to bring students, teachers
Applied Physics Laboratory                                                 and the public along on CONTOUR’s amazing ride of
Navigation and Deep Space Network (DSN) Support:                           scientific discovery. The program brings the thrill and
NASA Jet Propulsion Laboratory                                             wonder of exploring comets into classrooms and homes
Science Team:                                                              through Web sites, teacher and student workshops,
18 co-investigators from universities, industry and                        educational programs, electronic materials, professional
government agencies in the U.S. and Europe                                 and amateur astronomer involvement and media events.

                                          Visit CONTOUR on the Web: www.contour2002.org
                                                                                                                                   02- 0279

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Contour

  • 1. www.contour2002.org CONTOUR Tour Sun Earth Sc hw Comet Nucleus ass man n–Wachmann 3 A Mission to Study the Diversity of Comet Nuclei The CONTOUR mission is our most detailed MISSION PROFILE look yet at the heart of a comet — its nucleus. • Launch: July 2002 from Cape Canaveral Air Force CONTOUR will fly to within 100 kilometers (about Station, Florida, aboard a Delta II (7425) launch vehicle. 60 miles) of at least two comet nuclei, assessing their diversity and discovering how these primitive • Innovative Launch Concept: CONTOUR orbits building blocks of the solar system have evolved Earth for several weeks after launch, moving into position for maneuver sending it into a solar orbit since forming more than 4.5 billion years ago. on Aug. 15, 2002. Key Measurements • Close-up Encounters: Fly past and collect data on • Detailed imaging of the nucleus comets Encke (Nov. 2003) and Schwassmann- (4-meter resolution) Wachmann 3 (June 2006). • Spectral mapping of the nucleus (100- to 200-meter resolution) • Mission Flexibility: Earth swingbys (gravity-assist • Analysis of gas and dust surrounding maneuvers) refine trajectory for comet encounters or retarget spacecraft toward a “new” comet. the nucleus — Swingbys occur Aug. 2003; Aug. 2004; THE SPACECRAFT Feb. 2005; Feb. 2006. Simple and compact, CONTOUR has few hinged and • Minimal Operations Support: Spacecraft movable parts; a body-mounted solar array; and a spends 65% of flight in unattended, spin-stabilized mission geometry suitable for fixed, passive antennas. “hibernation.” Operators point the instruments and antennas by moving the spacecraft. A layered shield of Nextel and Kevlar protects CONTOUR from speeding dust and particles CONTOUR Remote Imager/Spectrograph (CRISP) • Takes high-resolution photos of nucleus near the nucleus. • Maps ice and rock types on surface • 8-sided body; 2 meters (6 feet) tall; 2 meters wide Mass: 26.7 kg (59 pounds) • Total weight: 970 kilograms (2,138 pounds) Power: 45 watts (average) — Dry spacecraft: 387 kilograms Supplier: Johns Hopkins University Applied Physics Laboratory — Solid rocket motor: 503 kilograms — Hydrazine fuel: 80 kilograms Dust Shield • Two modes of operation — Spin-stabilized cruise mode Neutral Gas and Ion Mass Spectrometer — Precision, 3-axis stabilized (NGIMS) encounter mode • Counts and analyzes atoms, molecules and ions around nucleus • Designed for solar distance Mass: 13.5 kg (30 pounds) up to 195 million kilometers Power: 47 watts (average) (about 121 million miles). Supplier: NASA/ • Two, 5-gigabit solid- Goddard Space Flight Center state data recorders Comet Impact Dust Analyzer (CIDA) Thruster Pods • Determines composition of (2 of 4) dust surrounding nucleus Mass: 10.5 kg (23 pounds) CONTOUR Forward Imager (CFI) Power: 13 watts (average) • Locates comet on approach Supplier: von Hoerner • Snaps color pictures of gas, dust jets near nucleus & Sulger, GmbH Mass: 9.7 kg (21 pounds) Power: 10 watts (average) Supplier: Johns Hopkins University Applied Physics Laboratory
  • 2. THE COMETS THE ENCOUNTERS CONTOUR’s target comets have CONTOUR first “sees” the target diverse physical characteristics and will comet several days before each be relatively close to Earth during each encounter, while the nucleus is still encounter. thousands of kilometers away. The Evolved yet active, Encke has been mission team then directs the craft observed at more apparitions (57) toward the comet and prepares to than any other comet, even Halley. gather data. Encke takes about 3 years to orbit the Timeline Sun. Encke has traveled this orbit for 48 seconds (1,350 kilometers) 60 to 10 days before encounter: thousands of years, so its continued The mission team determines the activity is rather puzzling. spacecraft’s position and checks out Schwassmann-Wachmann 3 was its systems and instruments. discovered in 1930. Its activity was 10 days to 12 hours before: predictable until the mid-1990s, when CONTOUR snaps pictures and makes it split into several pieces. When spectral observations of the coma. The CONTOUR reaches SW3 in 2006, images also help operators navigate the it could see relatively fresh, unaltered spacecraft. surfaces and evidence of materials inside 12 hours before to 12 hours after: the nucleus. CONTOUR is in full encounter mode; 20 seconds (475 kilometers) all instruments are turned on and A “New” Comet programmed to fill the spacecraft’s Should a new, scientifically data recorders. appealing comet reach the inner solar system during the mission, 12 hours to 15 days after: CONTOUR sends data back to Earth, CONTOUR can change its path and the mission team verifies the (after the Encke encounter) to spacecraft’s orbit. study it. The potential target should be active and bright — much like comet Hale-Bopp, THE CAMERA EYE which was prominent in 1997. A simulated look at Encke’s nucleus through CRISP, noting time and 8 seconds (260 kilometers) 1 astronomical unit (AU) is the average distance distance to closest approach. between Earth and the Sun, about 150 million kilometers (93 million miles). Sun Earth Flyby A NASA DISCOVERY MISSION Encounter Distance Distance Speed CONTOUR is the sixth mission in NASA’s innovative Date (AU) (AU) (km/sec) Discovery Program of low-cost, highly focused scientific Encke, 11/12/03 1.08 0.27 28.2 exploration projects. Other Discovery missions to small bodies include Near Earth Asteroid Rendezvous (NEAR) SW3, 6/19/06 0.96 0.32 14.0 — the first mission to orbit and land on an asteroid — the Stardust and Deep Impact comet studies, and the Dawn MISSION MANAGEMENT asteroid-orbiter mission. For more information visit Principal Investigator: http://discovery.nasa.gov. Dr. Joseph Veverka, Cornell University Project Management, Spacecraft Development EDUCATION AND PUBLIC OUTREACH and Mission Operations: The mission’s comprehensive Education and Public The Johns Hopkins University Outreach efforts are designed to bring students, teachers Applied Physics Laboratory and the public along on CONTOUR’s amazing ride of Navigation and Deep Space Network (DSN) Support: scientific discovery. The program brings the thrill and NASA Jet Propulsion Laboratory wonder of exploring comets into classrooms and homes Science Team: through Web sites, teacher and student workshops, 18 co-investigators from universities, industry and educational programs, electronic materials, professional government agencies in the U.S. and Europe and amateur astronomer involvement and media events. Visit CONTOUR on the Web: www.contour2002.org 02- 0279