Design guidelines for assessing and controlling spacecraft charging effects
Carolyn K. Purvis, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984 - Science - 42 pages
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Appendix A Description of Geosynchronous Plasma Environments
Voyager SEMCAP Analysis
Aeronaut AIAA ambient analysis antenna arc discharge arc source Astronaut blanket breakdown C. P. Pike cable capacitance capacitor charge control Charged Spacecraft Charging by Magnetospheric Charging Technology Conference circuit conductive Current density density for population differential charging electric fields electrostatic discharge energy ESD test European Space Agency Faraday cage flux Geophys Geosynchronous Orbit guidelines Guyenne IEEE Trans indium tin oxide Ionosphere Kapton Magnetospheric Plasmas Maxwell-Boltzmann Maxwell-Boltzmann distribution Maxwellian metal NASA TM NASCAP Nucl Number density oscilloscope parameters photoelectron Photon and Particle Pike and R. R. predicted Probe Prog proton Purvis R. R. Lovell radiated Satellite SCATHA Secondary Electron SEMCAP shield simulate solar array space plasma space vehicle spacecraft charging effects Spacecraft Charging Technology Spacecraft Charging Technology—1978 spacecraft potential spacecraft structure spacecraft surface specific structure current substorm environment surface charging Surface Discharges Surfaces in Space Teflon Temperature for population thermal transients Whipple wires