Methods and systems for mitigating or reducing the risk of an electrostatic discharge due to static charge differentials between a first spacecraft and a second spacecraft as the first spacecraft approaches the second spacecraft may be accomplished using a passive electrostatic discharge mitigation device. In some embodiments, mitigation of static potential between the first spacecraft and the second spacecraft may be actively accomplished by an electric propulsion system 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.
УМЕНЬШЕНИЕ РИСКА ВОЗНИКНОВЕНИЯ И ОСЛАБЛЕНИЕ ЭЛЕКТРОСТАТИЧЕСКОГО РАЗРЯДА ДЛЯ ПЕРВОГО КОСМИЧЕСКОГО АППАРАТА, РАБОТАЮЩЕГО ПОБЛИЗОСТИ ОТ ВТОРОГО КОСМИЧЕСКОГО АППАРАТА, И СВЯЗАННЫЕ С ЭТИМ СПОСОБЫ
2021-05-13
Patent
Elektronische Ressource
Russisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
СИСТЕМЫ ДЛЯ ЗАХВАТА КЛИЕНТСКОГО КОСМИЧЕСКОГО АППАРАТА И СВЯЗАННЫЕ СПОСОБЫ
Europäisches Patentamt | 2021
УСТРОЙСТВО АЭРОДИНАМИЧЕСКОГО ТОРМОЖЕНИЯ КОСМИЧЕСКОГО АППАРАТА
Europäisches Patentamt | 2018