ELECTROSTATIC DISCHARGE MITIGATION FOR A FIRST SPACECRAFT OPERATING IN PROXIMITY TO A SECOND SPACECRAFT

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...

Full description

Saved in:
Bibliographic Details
Main Authors Herbert, Gregg A, Agathon-Burton, Christine A, Llorens, William A, Graham, Ronald Lynn, Michel, Matthew Alan, Cochran, Dewey Edwin
Format Patent
LanguageEnglish
Published 18.10.2018
Subjects
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
Online AccessGet full text

Cover

More Information
Summary: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.
Bibliography:Application Number: US201715829758