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Double-lunar swingby trajectories for the spacecraft of the International Solar Terrestrial Physics programThe ISEE-3 satellite carried out the first extensive exploration of the distant geomagnetic tail during 1983. ISEE-3's orbit was altered with four lunar gravity assists that alternately decreased and increased its orbital energy while keeping the apogees aligned in the antisolar direction. Two spacecraft of the International Solar Terrestrial Physics program will use similar double-lunar swingby orbits to study the solar wind and the geomagnetic environment. Geotail will be built in Japan for the Institute of Space and Astronautical Sciences; its main purpose will be to explore the earth's geomagnetic tail. Wind is a NASA spacecraft that will monitor the solar wind upstream from the earth and will also study the bowshock region of the magnetosphere. Current plans call for launches of both by NASA with expendable launch vehicles during the second half of 1992.
Document ID
19900056451
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dunham, David W.
(Computer Sciences Corp. Lanham, MD, United States)
Jen, Shao-Chiang
(Computer Sciences Corp. Lanham, MD, United States)
Lee, Taesul
(Computer Sciences Corp. Lanham, MD, United States)
Swade, D.
(Computer Sciences Corp. Lanham, MD, United States)
Kawaguchi, Jun'ichiro
(Institute of Space and Astronautical Science Sagamihara, Japan)
Farquhar, Robert W.
(Computer Sciences Corp. Lanham, MD, United States)
Broaddus, S.
(Computer Sciences Corp. Lanham, MD, United States)
Engel, Cheryl
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Astrodynamics
Report/Patent Number
AAS PAPER 89-167
Meeting Information
Meeting: AAS/NASA Intl. Symposium on Orbital Mechanics and Mission Design
Location: Greenbelt, MD
Country: United States
Start Date: April 24, 1989
End Date: April 27, 1989
Accession Number
90A43506
Distribution Limits
Public
Copyright
Other

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