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
2005
Article (Journal)
English
BKL: | 55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung | |
Local classification TIB: | 770/3520/8000 |
Electric Polarization of Low-Orbit Spacecraft
Springer Verlag | 2005
|On-orbit spacecraft reliability
NTRS | 1978
|On-Orbit Spacecraft Reliability
NTIS | 1978
|