I.S. EN 16603-20-06:2014
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
View Superseded by
SPACE ENGINEERING - SPACECRAFT CHARGING
Hardcopy , PDF
31-03-2021
English
01-01-2014
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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.
| DocumentType |
Standard
|
| Pages |
122
|
| PublisherName |
National Standards Authority of Ireland
|
| Status |
Withdrawn
|
| 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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