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BSI BS EN 16603-20-06:2020

Space engineering. Spacecraft charging
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BSI BS EN 16603-20-06:2020

Space engineering. Spacecraft charging

PUBLISH DATE 2020
PAGES 128
BSI BS EN 16603-20-06:2020

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 behaviour.

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.

SDO BSI: British Standards Institution
Document Number EN 16603-20-06
Publication Date Nov. 19, 2020
Language en - English
Page Count 128
Revision Level
Supercedes
Committee ACE/68
Publish Date Document Id Type View
July 31, 2014 BS EN 16603-20-06:2014 Revision
Nov. 19, 2020 BS EN 16603-20-06:2020 Consolidated