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Norm

ÖNORM EN 16603-20-06

Issue date: 2014 10 01

Space engineering - Spacecraft charging

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 t...
Withdrawn: 2020 11 01
Publisher:
Austrian Standards International
Format:
Digital | 120 Pages
Language:
English
Optionally co-design standards:
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.
ÖVE/ÖNORM EN 16603-20-06
2020 11 01
Space engineering - Spacecraft charging
Norm
ÖNORM EN 16603-20-06
2014 10 01
Space engineering - Spacecraft charging
Norm
Norm
ÖNORM EN 16601-00-01
Issue date : 2015 03 15
Space systems - Glossary of terms
Norm
ÖVE/ÖNORM EN 16603-20-06
Issue date : 2020 11 01
Space engineering - Spacecraft charging