ISO 16127:2014
Withdrawn
View Superseded by
Space systems — Prevention of break-up of unmanned spacecraft
Hardcopy , PDF
English
02-13-2014
04-09-2025
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.
| Committee |
ISO/TC 20/SC 14
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| 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Withdrawn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 |
| ISO 16164:2015 | Space systems — Disposal of satellites operating in or crossing Low Earth Orbit |
| 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 |
| ISO/TR 20590:2017 | Space systems - Debris mitigation design and operation manual for launch vehicle orbital stages |
| BS ISO 26872:2010 | Space systems. Disposal of satellites operating at geosynchronous altitude |
| BS ISO 16164:2015 | Space systems. Disposal of satellites operating in or crossing Low Earth Orbit |
| 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 |
| ISO 24638:2008 | Space systems — Pressure components and pressure system integration |
| ISO 10795:2011 | Space systems — Programme management and quality — Vocabulary |
| MIL-STD-1522 Revision A:1984 | Standard General Requirements for Safe Design and Operation of Pressurized Missile and Space Systems |
| ISO 24113:2011 | Space systems — Space debris mitigation requirements |
| ISO 21347:2005 | Space systems — Fracture and damage control |
| ISO 17666:2016 | Space systems — Risk management |
| ISO 14623:2003 | Space systems - Pressure vessels and pressurized structures — Design and operation |
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