HR: 1340h
AN: P23A-0249    [Abstracts]
TI: The MESSENGER Payload
AU: * Gold, R E
EM: robert.gold@jhuapl.edu
AF: The Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Road, Laurel, MD 20723 United States
AU: Solomon, S C
AF: Department of Terrestrial Magnetism, Carnegie Institution of Washington, 5241 Broad Branch Road, N.W., Washington, DC 20015 United States
AU: McNutt, R L
AF: The Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Road, Laurel, MD 20723 United States
AU: Leary, J C
AF: The Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Road, Laurel, MD 20723 United States
AB: The MErcury, Surface, Space ENvironment, GEochemistry, and Ranging (MESSENGER) spacecraft, launched on 3 August 2004, will be the first orbiter of the planet Mercury. After insertion into a near-polar Mercury orbit in March 2011 MESSENGER will make detailed measurements of the planet for one Earth year. During the 6.6-year cruise phase, MESSENGER will fly by Mercury three times and map $>$90% of the planet. The payload consists of seven instruments, including a dual imaging system with wide-angle and narrow-angle cameras; an integrated ultraviolet, visible, and infrared spectrometer that is sensitive enough to detect atmospheric emissions and robust enough to map spectral absorption features on the sun-lit surface; gamma-ray, neutron, and X-ray spectrometers for remote geochemical mapping; a vector magnetometer to examine the internal and external field sources; a laser altimeter to examine the topography of surface features and determine whether Mercury has a fluid core; and an energetic particle and plasma spectrometer to characterize ionized species in the magnetosphere. The payload was fully calibrated before launch, and all instruments have been successfully operated in space. An Earth flyby one year after launch will be used for extensive in-flight calibration, and two Venus flybys will provide further opportunities for instrument observations. The MESSENGER spacecraft and instruments must cope with the $>$14 kWm$^{-2}$ solar thermal input and the large velocity change required to reach and survive in Mercury orbit. Several unique technologies have made this mission possible.
DE: 5464 Remote sensing
DE: 5494 Instruments and techniques
SC: Planetary Sciences [P]
MN: 2004 AGU Fall Meeting