TY - JOUR
T1 - Remote sensing of a comet at millimeter and submillimeter wavelengths from an orbiting spacecraft
AU - Gulkis, Samuel
AU - Allen, Mark
AU - Backus, Charles
AU - Beaudin, Gérard
AU - Biver, Nicolas
AU - Bockelée-Morvan, Dominique
AU - Crovisier, Jacques
AU - Despois, Didier
AU - Encrenaz, Pierre
AU - Frerking, Margaret
AU - Hofstadter, Mark
AU - Hartogh, Paul
AU - Ip, Wing
AU - Janssen, Mike
AU - Kamp, Lucas
AU - Koch, Timothy
AU - Lellouch, Emmanuel
AU - Mann, Ingrid
AU - Muhleman, Duane
AU - Rauer, Heike
AU - Schloerb, Peter
AU - Spilker, Thomas
PY - 2007/6
Y1 - 2007/6
N2 - The ESA Rosetta Spacecraft, launched on March 2, 2004 with the ultimate destination being Comet 67P/Churyumov-Gerasimenko, carries a relatively small and lightweight millimeter-submillimeter spectrometer instrument, the first of its kind launched into deep space. The instrument, named Microwave Instrument for the Rosetta Orbiter (MIRO), consists of a 30-cm diameter, offset parabolic reflector telescope, which couples energy in the millimeter and submillimeter bands to two heterodyne receivers. Center-band operating frequencies are near 190 GHz (1.6 mm) and 562 GHz (0.5 mm). Broadband, total power continuum measurements can be made in both bands. A 4096-channel spectrometer with 44 kHz resolution is connected to the submillimeter receiver. The spectral resolution is sufficient to observe individual, thermally broadened spectral lines (T≥10 K). The submillimeter radiometer/spectrometer is fixed tuned to measure four volatile species-CO, CH3OH, NH3 and three isotopes of water, H216O, H217O and H218O. The MIRO experiment will use these species as probes of the physical conditions within the nucleus and coma. The basic quantities measured by MIRO are surface temperature, gas production rates and relative abundances, and velocity and excitation temperature of each species, along with their spatial and temporal variability. This information will be used to infer coma structure and outgassing processes, including the nature of the nucleus/coma interface.
AB - The ESA Rosetta Spacecraft, launched on March 2, 2004 with the ultimate destination being Comet 67P/Churyumov-Gerasimenko, carries a relatively small and lightweight millimeter-submillimeter spectrometer instrument, the first of its kind launched into deep space. The instrument, named Microwave Instrument for the Rosetta Orbiter (MIRO), consists of a 30-cm diameter, offset parabolic reflector telescope, which couples energy in the millimeter and submillimeter bands to two heterodyne receivers. Center-band operating frequencies are near 190 GHz (1.6 mm) and 562 GHz (0.5 mm). Broadband, total power continuum measurements can be made in both bands. A 4096-channel spectrometer with 44 kHz resolution is connected to the submillimeter receiver. The spectral resolution is sufficient to observe individual, thermally broadened spectral lines (T≥10 K). The submillimeter radiometer/spectrometer is fixed tuned to measure four volatile species-CO, CH3OH, NH3 and three isotopes of water, H216O, H217O and H218O. The MIRO experiment will use these species as probes of the physical conditions within the nucleus and coma. The basic quantities measured by MIRO are surface temperature, gas production rates and relative abundances, and velocity and excitation temperature of each species, along with their spatial and temporal variability. This information will be used to infer coma structure and outgassing processes, including the nature of the nucleus/coma interface.
KW - Comets
KW - Spacecraft instruments
KW - Submillimeter spectroscopy
UR - http://www.scopus.com/inward/record.url?scp=34249282389&partnerID=8YFLogxK
U2 - 10.1016/j.pss.2006.11.011
DO - 10.1016/j.pss.2006.11.011
M3 - 期刊論文
AN - SCOPUS:34249282389
SN - 0032-0633
VL - 55
SP - 1050
EP - 1057
JO - Planetary and Space Science
JF - Planetary and Space Science
IS - 9
ER -