Physics
Scientific paper
Oct 1976
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1976stin...7723369g&link_type=abstract
Presented at the USAF/NASA Spacecraft Charging Technol. Conf., U.S. Air Force Acad., Colo., 27-29 Oct. 1976
Physics
Electric Potential, Electron Emission, Electron Sources, Spacecraft Environments, Cathodes, Earth Magnetosphere, Jupiter (Planet), Spacecraft Design
Scientific paper
The principles which govern the interaction of a spacecraft with its environment are recapitulated, and the various techniques available for controlling the electrostatic potential of a spacecraft are reviewed. It is demonstrated that electron emitters are requisite to any scientific mission in a magnetospheric environment, in the vicinity of Jupiter in particular. It is also emphasized that electron sources can be used simultaneously for a number of additional tasks such as monitoring the degradation of spacecraft material surfaces, converting the thermal motion of plasmas into electrical energy, measuring the density and temperature of the ambient electrons, and receiving waves without antennas.
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