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ISO 16127:2014

Space systems — Prevention of break-up of unmanned spacecraft

Feb 13, 2014
95.99 Withdrawal of Standard   Jul 14, 2022

General information

95.99     Jul 14, 2022

ISO

ISO/TC 20/SC 14

International Standard

49.140  

English  

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Scope

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.

Life cycle

NOW

WITHDRAWN
ISO 16127:2014
95.99 Withdrawal of Standard
Jul 14, 2022

REVISED BY

PUBLISHED
ISO 23312:2022