ISO 16127:2014
w
ISO 16127:2014
55721

Status : Withdrawn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

  •  : Withdrawn
     : 2014-02
    : Withdrawal of International Standard [95.99]
  •  : 1
     : 9
  • ISO/TC 20/SC 14
    49.140 
  • RSS updates

Got a question?

Check out our FAQs

Customer care
+41 22 749 08 88

Opening hours:
Monday to Friday - 09:00-12:00, 14:00-17:00 (UTC+1)