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ISO 16127:2014

Withdrawn
Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

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withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

Space systems — Prevention of break-up of unmanned spacecraft
Available format(s)

Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users

Withdrawn date

07-14-2022

Language(s)

English

Published date

02-13-2014

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.

DevelopmentNote
Supersedes ISO/DIS 16127. (02/2014)
DocumentType
Standard
Pages
9
ProductNote
THIS STANDARD ALSO REFERS TO ECSS-E-ST-32-02C rev 1,ANSI/AIAA S-080-1998,ANSI/AIAA S-081A-2006,ECSS-E-ST-35C rev 1,ECSS-E-ST-35-01C,
PublisherName
International Organization for Standardization
Status
Withdrawn
SupersededBy

Standards Relationship
BS ISO 16127:2014 Identical

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BS ISO 16699:2015 Space systems. Disposal of orbital launch stages
14/30213848 DC : 0 BS ISO 16164 - SPACE SYSTEMS - DISPOSAL OF SATELLITES OPERATING IN OR CROSSING LOW EARTH ORBIT
ISO 16699:2015 Space systems Disposal of orbital launch stages
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BS ISO 26872:2010 Space systems. Disposal of satellites operating at geosynchronous altitude
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PD ISO/TR 18146:2015 Space systems. Space debris mitigation design and operation guidelines for spacecraft
ISO 26872:2010 Space systems Disposal of satellites operating at geosynchronous altitude
ISO/TR 18146:2015 Space systems Space debris mitigation design and operation guidelines for spacecraft
PD ISO/TR 20590:2017 Space systems. Debris mitigation design and operation manual for launch vehicle orbital stages

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ISO 17666:2016 Space systems — Risk management
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