Abstract The main problems concerning the electric polarization of low-orbit spacecraft are considered, including the results of studying the structure of the Earth's upper ionosphere, the methods of calculating the electrophysical characteristics of construction materials for spacecraft, and the elaboration of recommendations to mitigate the negative effects due to processes of charging and discharging.
Electric Polarization of Low-Orbit Spacecraft
Cosmic Research ; 43 , 6 ; 432-441
2005-11-01
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Electric Polarization of Low-Orbit Spacecraft
Online Contents | 2005
|On-Orbit Spacecraft Reliability
NTIS | 1978
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