ECSS-E-ST-20-06C Rev.1 – Spacecraft charging (15 May 2019)

This Standard cancels and replaces ECSS-E-ST-20-06C (31 July 2008)




This standard is a standard within the ECSS hierarchy. It forms part of the electrical and electronic engineering discipline (ECSS-E-ST-20) of the engineering branch of the ECSS system (ECSS-E). It provides clear and consistent provisions to the application of measures to assess, in order to avoid and minimize hazardous effects arising from spacecraft charging and other environmental effects on a spacecraft’s electrical behavior.

This standard is applicable to any type of spacecraft including launchers, when above the atmosphere.

Although spacecraft systems are clearly subject to electrical interactions while still on Earth (e.g. lightning and static electricity from handling), these aspects are not covered, since they are common to terrestrial systems and covered elsewhere. Instead this standard covers electrical effects occurring in space (i.e. from the ionosphere upwards).

This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.



Md5 checksum .docx file = 0674E07B903F42B1FB5741C7723A0EE9
Md5 checksum .pdf file = BEC8E88B405C48482AD01A1BC96F1FB7

See also the new Handbook ECSS-E-HB-20-06A “Assessment of space worst case charging handbook” (15 May 2019)