BS ISO 19923:2017
Current
The latest, up-to-date edition.
Space environment (natural and artificial). Plasma environments for generation of worst case electrical potential differences for spacecraft
Hardcopy , PDF
English
28-06-2017
Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Symbols and abbreviated terms
5 Criteria for worst-case environment
6 Procedures for application to spacecraft design
7 Space environments for worst-case simulations
Annex A (informative) - Spacecraft charging analysis
tools
Annex B (informative) - Round-robin simulation
Annex C (normative) - Material properties
Annex D (informative) - Tailoring guideline for this
document
Bibliography
Describes space plasma environments that lead to the generation of the worst-case surface potential differences for spacecraft.
Committee |
ACE/68
|
DevelopmentNote |
Supersedes 16/30311284 DC. (07/2017)
|
DocumentType |
Standard
|
Pages |
22
|
PublisherName |
British Standards Institution
|
Status |
Current
|
Supersedes |
This document specifies space plasma environments that lead to the generation of the worst-case surface potential differences for spacecraft. It also specifies how to estimate worst-case potential differences by using the simulation codes provided.
This document includes plasma energy and density in GEO, PEO, and MEO. This document does not include descriptions of plasma energy and density in LEO because large surface charging in LEO is likely to be due to high-voltage power generation by instrumentation of the spacecraft.
This document deals with external surface charging of spacecraft only.
Standards | Relationship |
ISO 19923:2017 | Identical |
ISO 10795:2011 | Space systems Programme management and quality Vocabulary |
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