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Geotail

Geotail [ISAS]

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.

Geotail is a spin-stabilized spacecraft utilizing mechanically despun antennas with a design lifetime of about four years. The nominal spin rate of the spacecraft is about 20 rpm around a spin axis maintained between 85-89 degrees to the ecliptic plane. Geotail is cylindrical, approximately 2.2 m in diameter and 1.6 m high with body-mounted solar cells. Geotail also has a back-up battery subsystem which operates when the spacecraft is in the Earth's shadow (limited to 2 hrs).

Real-time telemetry data transmitted in X-band are received at the Usuda Deep Space Center (UDSC) in Japan. There are two tape recorders on board, each with a capacity of 450 Mb which allows daily 24-hour data coverage and are collected in playback mode by the NASA Deep Space Network (DSN).

The Geotail mission is divided into two phases. During the two-year initial phase, the orbit apogee was kept on the nightside of the Earth by using the Moon's gravity in a series of double-lunar-swing-by maneuvers that result in the spacecraft spending most of its time in the distant magnetotail (maximum apogee about 200 Earth radii) with a period varying from one to four months. Then, starting in November 1994, there were a series of maneuvers to bring the spacecraft into its near-Earth orbit. This transition orbit lasted about three months with the apogee varying from 50 RE to 30 RE. The second phase is dedicated to the study of near-Earth neutral line formation.

Following instruments are mounted on the spacecraft:

  • Plasma Wave Investigation (PWI)
  • Energetic Particles and Ion Composition (EPIC)
  • Electric Field Detector (EFD)
  • Magnetic Fields Measurement (MGF)
  • Low Energy Particles (LEP) Dr. Toshifumi Mukai
  • Comprehensive Plasma Instrument (CPI)
  • High Energy Particles (HEP)
Nation: Japan, USA
Type / Application: Magnetosphere
Operator: ISAS, NASA
Contractors: ?
Equipment: PWI, EPIC, EFD, MGF, LEP, CPI, HEP
Configuration: ?
Propulsion: ?
Power: Solar cells, batteries
Lifetime:
Mass: 1009 kg
Orbit: 57000 km × 200000 km, 29
Satellite COSPAR Date LS Launch Vehicle Remarks
Geotail 1992-044A 24.07.1992 CC LC-17A Delta-6925 with DUVE

References:

Further ISTP missions: