BS ISO 15862:2009
Current
The latest, up-to-date edition.
Space systems. Launch-vehicle-to-spacecraft flight environments telemetry data processing
Hardcopy , PDF
English
31-03-2009
Foreword
Introduction
1 Scope
2 Terms and definitions
3 Abbreviated terms
4 Flight environments, measurement fields and
measurement requirements
5 Data processing and analysis
6 Analysis results reports of flight environments
Gives basic requirements for the measurement of the spacecraft flight environments generated by the launch vehicle, telemetry data processing and formats of analysis reports.
Committee |
ACE/68
|
DevelopmentNote |
Supersedes 08/30176277 DC. (03/2009)
|
DocumentType |
Standard
|
Pages |
18
|
PublisherName |
British Standards Institution
|
Status |
Current
|
Supersedes |
This International Standard provides basic requirements for the measurement of the spacecraft flight environments generated by the launch vehicle, telemetry data processing and formats of analysis reports.
This International Standard defines the field and number of measurement parameters, the principles of data processing, the format of delivered data and the content and the form of the flight environment analysis report.
Flight telemetry data are used to verify if flight environment conditions exceed pre-flight analyses and environmental test results. In the event of a launch failure, adequate flight environment data can assist in investigating and analysing failure causes.
This International Standard is applicable to commercial launch vehicles and related ground processing, no matter which launch vehicle agencies are selected.
Standards | Relationship |
ISO 15862:2009 | Identical |
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