Status : Withdrawn

This standard has been revised by ISO 23312:2022

Abstract

ISO 16127:2014 defines the requirements to reduce the risk of in-orbit break-up of unmanned spacecraft, both during and after their operational lives. The aim would be met by reducing the possibility of a break-up caused by an unplanned internally caused event and by depleting to a safe level all the sources of stored energy at the end of a spacecraft's life. ISO 16127:2014 is designed for use in planning, verifying and implementing the prevention of break-up of a spacecraft.

ISO 16127:2014 applies only to unmanned spacecraft operating in Earth orbit.

General information

  • Status
     : Withdrawn
    Publication date
     : 2014-02
    Stage
    : Withdrawal of International Standard [95.99]
  • Edition
     : 1
    Number of pages
     : 9
  • Technical Committee :
    ISO/TC 20/SC 14
    ICS :
    49.140 
  • RSS updates

Life cycle

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal

9
Industry, Innovation and Infrastructure

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