International Standard
ISO 15862:2009
Space systems — Launch-vehicle-to-spacecraft flight environments telemetry data processing
Reference number
ISO 15862:2009
Edition 1
2009-02
International Standard
Read sample
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ISO 15862:2009
42033
Published (Edition 1, 2009)
This standard was last reviewed and confirmed in 2020. Therefore this version remains current.

ISO 15862:2009

ISO 15862:2009
42033
Format
Language
CHF 63
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Abstract

ISO 15862:2009 provides basic requirements for the measurement of the spacecraft flight environments generated by the launch vehicle, telemetry data processing and formats of analysis reports.

ISO 15862:2009 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.

ISO 15862:2009 is applicable to commercial launch vehicles and related ground processing, no matter which launch vehicle agencies are selected.

General information

  •  : Published
     : 2009-02
    : International Standard confirmed [90.93]
  •  : 1
     : 9
  • ISO/TC 20/SC 14
    49.140 
  • RSS updates

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