Space systems. Launch-vehicle-to-spacecraft flight environments telemetry data processing

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

31-03-2009

Publisher

British Standards Institution

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.

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.

Committee	ACE/68
DevelopmentNote	Supersedes 08/30176277 DC. (03/2009)
DocumentType	Standard
Pages	18
PublisherName	British Standards Institution
Status	Current
Supersedes	08/30176277 DC : DRAFT JAN 2008

Standards	Relationship
ISO 15862:2009	Identical

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BS ISO 15862:2009

Space systems. Launch-vehicle-to-spacecraft flight environments telemetry data processing

Table of Contents

Abstract

Scope

General Product Information

International Equivalents

Category

Subcategory