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From Wikipedia, the free encyclopedia

Geotail
Geotail satellite.jpg
Geotail satellite (artist's concept)
Mission typeEarth observation
OperatorISAS / NASA
COSPAR ID1992-044A
SATCAT no.22049
Websitewww.stp.isas.jaxa.jp/geotail/
Mission duration20 years (planned)
Spacecraft properties
Launch mass980 kg (2,160 lb)
Power273.0 watts
Start of mission
Launch date24 July 1992, 14:26:00 (1992-07-24UTC14:26Z) UTC
RocketDelta II 6925
Launch siteCape Canaveral LC-17A
Orbital parameters
Reference systemGeocentric
RegimeHEO
Semi-major axis127,367.75 km (79,142.65 mi)[1]
Eccentricity0.5469845[1]
Perigee altitude51,328 km (31,894 mi)[1]
Apogee altitude190,664 km (118,473 mi)[1]
Inclination10.51 degrees[1]
Period7539.86 minutes[1]
Epoch15 January 2015, 13:40:53 UTC[1]
 

Geotail is a satellite observing the Earth's magnetosphere. It was developed by Japan's ISAS in association with the United States' NASA, and was launched by a Delta II rocket on 24 July 1992 from Cape Canaveral Air Force Station.

The primary purpose of this mission is to study the structure and dynamics of the tail region of the magnetosphere with a comprehensive set of scientific instruments. For this purpose, the orbit has been designed to cover the magnetotail over a wide range of distances: 8 R to 210 R from the earth. This orbit also allowed it to study the boundary region of the magnetosphere as it skims the magnetopause at perigees. In the first two years the double lunar swing-by technique was used to keep apogees in the distant magnetotail. This involved 14 lunar flybys.[2]

In 1993 the computer that controls the Low Energy Particles experiment locked up.[2] Attempts to reset it failed.[2] This problem was solved by changing the trajectory of the craft during a lunar flyby that took place on 26 September 1993 so that it passed through the shadow of the moon.[2] Power from the batteries was cut while this took place.[2] When the craft left the shadow of the moon, power returned and the computer started working again.[2]

The apogee was lowered down to 50 R in mid November 1994 and then to 30 R in February 1995 in order to study substorm processes in the near-Earth tail region. The present orbit is 9 R × 30 R with inclination of -7° to the ecliptic plane."

Geotail instruments studied electric fields, magnetic fields, plasmas, energetic particles, and plasma waves.[3]

In 1994 the principal investigator of the Plasma Wave Instrument (PWI), the experiment complement, was Professor Hiroshi Matsumoto of Kyoto University, with co-investigators from NASA, the University of Iowa, and STX Corporation.[4] Geotail is an active mission as of 2021.[5] Geotail, WIND, Polar, SOHO, and Cluster were all part of the International Solar-Terrestrial Physics Science Initiative (ISTP) project.[5]

Discoveries

Geotail data has been used to show that flux transfer events move faster than the ambient medium through the Magnetosphere.[6] Those within the Magnetosheath were shown to move both faster and slower than the ambient medium.[6]

During the lunar flybys Geotail identified oxygen, silicon, sodium and aluminium in the lunar atmosphere.[2]

See also

References

  1. ^ a b c d e f g "GEOTAIL Satellite details 1992-044A NORAD 22049". N2YO. 15 January 2015. Retrieved 25 January 2015.
  2. ^ a b c d e f g Ulivi, Paolo; Harland, David M (2004). Lunar Exploration Human Pioneers and Robot Surveyors. Springer. pp. 256–257. ISBN 185233746X.
  3. ^ Instruments of the Geotail Spacecraft Archived 3 September 2012 at the Wayback Machine
  4. ^ "The Geotail Plasma Wave Instrument". www-pw.physics.uiowa.edu. Retrieved 19 October 2014.
  5. ^ a b NASA - Geotail
  6. ^ a b Korotova, G.I.; Sibeck, D.G.; Rosenberg, T. (2009). "Geotail observations of FTE velocities" (PDF). Annales Geophysicae. Copernicus Publications. 27 (1): 83–92. Retrieved 26 April 2015.

External links

This page was last edited on 12 February 2021, at 11:22
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