Spacecraft charging can occur when a spacecraft vehicle is subject to space plasma environments and varying sunlit conditions. The trajectory of the spacecraft will determine the specific impinging environment while the spacecraft geometry and material properties determine the susceptibility to various charging issues. In general, spacecraft charging is separated into two categories, surface charging (~<100 keV) and internal charging (~>100keV).
Spacecraft Charging during Docking Operations in the Outer Radiation Belt
Applied Space Environments Conference ; 2019 ; Los Angeles, CA, United States
2019-05-14
Conference paper
No indication
English
Outer Radiation Belt Variations during 1995
British Library Conference Proceedings | 1998
|Outer Radiation Belt Variations during 1995
Online Contents | 1998
|DEVICE FOR AUTOMATIC DOCKING OF SPACECRAFT DURING ORBITAL SERVICE OPERATIONS
European Patent Office | 2018
|