GEOTAIL
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The GEOTAIL mission is a collaboration between the Japanese and American Space Adminstrations to study the dynamics of the Earth's magnetotail from the near-Earth region (8 Earth radii (Re)) to the distant geomagnetic tail (about 200 Re). The GEOTAIL spacecraft was designed and built by the Japanese and was launched on July 24, 1992. The Institute has contributed the HEP-LD designed to study plasma dynamics in the geomagnetic tail, solar flare particle acceleration and propagation, and the origin, lifetime and propagation of cosmic ray particles.
The Geotail mission measures global energy flow and transformation in the magnetotail to increase understanding of fundamental magnetospheric processes. This includes the physics of the magnetopause, the plasma sheet, and reconnection and neutral line formation (i.e., the mechanisms of input, transport, storage, release and conversion of energy in the magnetotail). Geotail, together with Wind, Polar, SOHO, and Cluster projects, constitute a cooperative scientific satellite project designated the International Solar-Terrestrial Physics (ISTP) program which aims at gaining improved understanding of the physics of solar terrestrial relations.
The Geotail mission is divided into two phases. During the initial two-year phase, the orbit apogee was kept on the night side of the Earth by using the Moon's gravity in a series of double-lunar-swing-by maneuvers that resulted in the spacecraft spending most of its time in the distant magnetotail (maximum apogee about 200 Re) with a period varying from one to four months. In February 1995, phase two was commenced as the apogee was reduced to 30 Re to study the near-Earth magnetotail processes.
The HEP-LD sensor system consists of three identical Imaging Ion Mass spectrometers which use time-of-flight/energy measurement, and covers 180 degrees in polar angle over the energy range 10--100 keV for ENA (Neutral Particles), 30 keV--1.5 MeV for Protons, 80keV--1.5 MeV for Helium ions, and 160 keV -- 4.0 MeV for CNO (Oxygen) Ions.
The instrument is not sensitive to the ionic charge state of nuclear particles; the mass resolution is marginal for separating carbon, nitrogen and oxygen ions. HEP-LD provides distribution of different ions with complete coverage of the unit sphere in phase space.
Flight Path S Deflection Voltage |
34 mm 0-10 KV |
Energy Range (KeV) Hydrogen Helium CNO |
30-1500 80-1500 160-4000 |
Angular Coverage: polar azimuthal |
180/12 360/16 |
ENA (KeV) | 10-100 |
Geomatric Factor total/differential |
0.24/0.02 |
By using the HEP-LD data sets, the following scientific objectives are investigating:
Geotail publications by MPS members | |
ISTP Home Page | |
Geotail Homepage | |
Geotail EPIC Summary Plots | |
GeoTail Comprehensive Plasma Instrument Observations |
© 2006, Max Planck Institute for Solar System Research, Lindau |
P. W. Daly 19-11-2001 |