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Dawn (Discovery 9)

Dawn [NASA]

Dawn is a NASA mission to journey to the two oldest and most massive objects in the asteoid belt, astreoid 4 Vesta and dwarf planet 1 Ceres.

Dawn will be the first purely scientific mission to be powered by ion propulsion, an advanced technology successfully demonstrated by NASA's Deep Space 1 mission. The use of solar electric ion thrusters will enable Dawn to orbit both asteroids in one mission, a feat that has not been attempted before.

Planned originally for launch in May 2006, Dawn was to reach, after a Mars fly-by, 4 Vesta in 2010 and 1 Ceres in 2014. In late 2005, the Dawn mission was delayed to a 2007 launch date instead of the planned June 2006 launch, due to ongoing concerns of the ion engines.

Dawn's science instruments investigate:

  • Internal structure, density and homogeneity of two complementary protoplanets, 1 Ceres and 4 Vesta, one wet and one dry
  • Determine shape, size, composition and mass
  • Surface morphology, cratering, magnetism
  • Determine thermal history and size of core
  • Understand role of water in controlling asteroid evolution
  • Test the current paradigm of Vesta as the howardite, eucrite, and diogenite (HED) parent body and determine which, if any, meteorites come from Ceres
  • Provide a geologic context for HEDs

The science payload consists of:

  • Framing Camera
  • Mapping Spectrometer
  • Gamma Ray and Neutron Spectrometer

A Laser Altimeter and a Magnetometer were dropped from the sensor suite during development.

Dawn has been cancelled in February 2006, when the spacecraft was nearly completed. On March, 27th 2006, Dawn was reinstated for a launch in 2007.

After launching in 2007, the Dawn spacecraft reached its first target, the asteroid Vesta in the main belt of asteroids between Mars and Jupiter, in July 2011. After spending 14 months surveying Vesta, Dawn was prepared to depart for Ceres in 2012, with two reaction wheels had suffered crippling malfunctions. In March 2015, Dawn entered an orbit around Ceres.

Nation: USA
Type / Application: Multiple asteroid orbiter
Operator: NASA
Contractors: Orbital Sciences Corporation (OSC)
Equipment: Framing Camera, Mapping Spectrometer, Gamma Ray and Neutron Spectrometer
Configuration:
Propulsion: 3 × NSTAR xenon ion engines
Power: 2 deployable solar arrays, batteries
Lifetime:
Mass: 1108 kg
Orbit: Heliocentric, later orbit around Vesta and Ceres
Satellite COSPAR Date LS Launch Vehicle Remarks
Dawn (Discovery 9) 2007-043A 27.09.2007 CC SLC-17B Delta-7925H

References: