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BS EN 16603-20-06:2014

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Space engineering. Spacecraft charging
Available format(s)

Hardcopy , PDF

Superseded date

19-11-2020

Language(s)

English

Published date

31-07-2014

Publisher

British Standards Institution

Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 Overview
5 Protection programme
6 Surface material requirements
7 Secondary arc requirements
8 High voltage system requirements
9 Internal parts and materials requirements
10 Tether requirements
11 Electric propulsion requirements
Annex A (normative) - Electrical hazard mitigation
        plan - DRD
Annex B (informative) - Tailoring guidelines
Annex C (informative) - Physical background to the
        requirements
Annex D (informative) - Charging simulation
Annex E (informative) - Testing and measurement
References
Bibliography

Gives 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 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.

Committee
ACE/68
DocumentType
Standard
Pages
124
PublisherName
British Standards Institution
Status
Superseded
SupersededBy

Standards Relationship
EN 16603-20-06:2014 Identical

EN 16603-35-01:2014 Space engineering - Liquid and electric propulsion for spacecraft
NASA HDBK 4002 : 2011 MITIGATING IN-SPACE CHARGING EFFECTS - A GUIDELINE
EN 16603-20-08:2014 Space engineering - Part 20-08: Photovoltaic assemblies and components
EN 16603-20-07:2014 Space engineering - Electromagnetic compatibility
EN 16602-70-71:2016 Space product assurance - Materials, processes and their data selection
EN 16603-10-04:2015 Space engineering - Space environment
EN 16601-00-01:2015 Space systems - Glossary of terms
EN 16603-35:2014 Space engineering - Propulsion general requirements
ISO 14302:2002 Space systems Electromagnetic compatibility requirements
ASTM D 257 : 2014 : REDLINE Standard Test Methods for DC Resistance or Conductance of Insulating Materials
EN 16603-10-03:2014 Space engineering - Testing
EN 16603-10-12:2014 Space engineering - Method for the calculation of radiation received and its effects, and a policy for design margins

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PDF - English
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