Methods and systems for mitigating or reducing the risk of an electrostatic discharge due to static charge differentials between a first spacecraft (10) and a second spacecraft (11) as the first spacecraft approaches the second spacecraft may be accomplished using a passive electrostatic discharge mitigation device (20). In some embodiments, mitigation of static potential between the first spacecraft and the second spacecraft may be actively accomplished by an electric propulsion system (31) provided on the first spacecraft. In some embodiments, mitigation may be provided by both actively and passively mitigating static potential between the first spacecraft and the second spacecraft.
Electrostatic discharge mitigation for a first spacecraft operating in proximity to a second spacecraft and related methods
2024-05-09
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Europäisches Patentamt | 2024
|Europäisches Patentamt | 2018
|Europäisches Patentamt | 2024
|Europäisches Patentamt | 2018
|Europäisches Patentamt | 2024
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