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- Path: sparky!uunet!usc!cs.utexas.edu!sun-barr!sh.wide!yscvax!yamada
- From: yamada@yscvax.ysc.go.jp (Yoshiro Yamada)
- Newsgroups: sci.space
- Subject: GEOTAIL MISSION
- Keywords: geotail, isas
- Message-ID: <1444@yscvax.ysc.go.jp>
- Date: 22 Jul 92 06:45:06 GMT
- Organization: Yokohama Science Center, Yokohama, JAPAN
- Lines: 89
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- * GEOTAIL *
-
-
- The GEOTAIL spacecraft is Japan's largest scientific satellite to date.
-
- The purpose of the GEOTAIL mission is to study the mechanism of
- input, transport, storage, release and conversion of energy in the magnetotail
- of the Earth. Part of the energy released produces very beautiful emission of
- light known as Aurora seen in the Antarctica and Arctic.
-
- The GEOTAIL spacecraft carries on board the following scientific
- instruments on board:
-
-
- Electric field detector,
-
- Magnetic field detector,
-
- Low energy plasma analyzer and ion mass spectrometer,
-
- Hot plasma analyzer and ion composition analyzer (from U.S.),
-
- High energetic particle detector,
-
- Energetic particles and ion composition spectrometer (from U.S.),
-
- and Plasma wave analyzer.
-
-
-
- The GEOTAIL spacecraft is a spin stabilized spacecraft utilizing
- a despun antennas system. The diameter of the spacecraft is approximately
- 2.2 meters with a height of 1.6 meters. The weight of the spacecraft
- is approximately 1,000 kg including 332 kg of hydrazine fuel. The design life
- is three years.
-
-
-
- The GEOTAIL will be launched from KSC by making use of Delta-II rocket
- into a 185 km circular parking orbit with an inclination of 28.7 degrees.
- The upper stage will be ignited to boost GEOTAIL into a translunar orbit.
- It is a unique point that the GEOTAIL changes its orbit by using the swingby
- and maneuver technique. Following are description of the phases of the
- GEOTAIL mission.
-
-
- (1) Translunar Phase (until L+50 days)
-
- Translunar phase is defined until the first lunar swingby,
- which takes place on September 8-th, 1992.
-
-
- (2) Distant Tail Phase (L+50 days to 1.78 years)
-
- The GEOTAIL spacecraft will be first injected onto distant tail orbit
- so that the orbital apsis should be aligned toward midnight side of the Earth.
- The orbital plane is almost same as that of the moon.
-
-
- (3) Trans-near-tail Phase (L+ 1.78 years to 1.85 years)
-
- This is corresponding to the period from the last swingby to the
- injection into near tail orbit. During this, two large amount of corrective
- maneuvers are carried out. One of them is the orbital plane change maneuver
- and the other is for the reduction of the apogee. The insertion
- into Near Tail Phase is scheduled in May, 1994.
-
-
- (4) Near Tail Phase (L+ 1.85 years to L+ 3.3 years)
-
- The second half of the scientific observation will be performed
- in the near tail phase, whose orbit is scheduled as 8 X 30 Re ellipse
- inclined 7.5 deg. to the ecliptic plane. The apogee is directed to antisunward
- at the June solstice. This phase will last at least one and half years.
-
-
-
- * All information is provided by the Office of External Relations;
- The Institute of Space and Astronautical Science
- 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229, Japan
-
- --
- -*--*--*--*--*--*--*--*--*--*--*--*--*--*--*--*--*--*--*--*--*--*---
- Yoshiro Yamada | tel : +81-45-832-1166
- Astronomy Section | fax : +81-45-832-1161
- Yokohama Science Center | e-mail : yamada@ysc.go.jp
-