Physics
Scientific paper
Oct 1981
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981motc.conf..277r&link_type=abstract
In JPL Mod. Observational Tech. for Comets p 277-283 (SEE N82-13989 04-89)
Physics
1
European Space Programs, Japanese Space Program, Mission Planning, U.S.S.R. Space Program, Flyby Missions, Instrument Packages, Orbital Elements, Spacecraft Configurations, Spacecraft Trajectories
Scientific paper
The 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.
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