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Plans for Comet HalleyThe configuration, trajectories, and payloads of a spinning Earth-orbiting satellite designed by ESA for a post-perihelion flythrough (Giotto mission) of Comet Halley are described. Experiments approved for use on two identical three-axis stabilized Venera spacecraft destined to encounter the comet after releasing probes to Venus are listed as well as the instruments to be carried on Japan's Planet-A flyby mission. The main features launch windows are given for each spacecraft.
Document ID
19820006151
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rahe, J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1981
Publication Information
Publication: JPL Mod. Observational Tech. for Comets
Subject Category
Astronomy
Accession Number
82N14024
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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