ISO 16127:2014
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
View Superseded by
Space systems — Prevention of break-up of unmanned spacecraft
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
14-07-2022
English
13-02-2014
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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)
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| DocumentType |
Standard
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| Pages |
9
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| 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,
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| PublisherName |
International Organization for Standardization
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| Status |
Withdrawn
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| 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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