ISO 26872:2010
Withdrawn
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View Superseded by
Space systems Disposal of satellites operating at geosynchronous altitude
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05-07-2019
English
03-09-2010
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ISO 26872:2010 specifies requirements for the following:
- planning for disposal of satellites operating at geosynchronous altitude to ensure that final disposal is sufficiently characterized and that adequate propellant will be reserved for the manoeuvre;
- selecting final disposal orbits where the satellite will not re-enter the operational region within the next 100 years;
- executing the disposal manoeuvre successfully;
- depleting all energy sources on board the vehicle before the end of its life to minimize the possibility of an event that can produce debris.
ISO 26872:2010 provides techniques for planning and executing the disposal of space hardware that reflect current internationally accepted guidelines and consider current operational procedures and best practices.
| DevelopmentNote |
Supersedes ISO/DIS 26872. (09/2010)
|
| DocumentType |
Standard
|
| Pages |
53
|
| PublisherName |
International Organization for Standardization
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| SAC GB/T 32308 : 2015 | Identical |
| BS ISO 26872:2010 | Identical |
| PD ISO/TR 18146:2015 | Space systems. Space debris mitigation design and operation guidelines for spacecraft |
| BS ISO 16699:2015 | Space systems. Disposal of orbital launch stages |
| 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 23339:2010 | Space systems. Unmanned spacecraft. Estimating the mass of remaining usable propellant |
| ISO 23339:2010 | Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant |
| 13/30235933 DC : 0 | BS ISO 16699 - SPACE SYSTEMS - DISPOSAL OF ORBITAL LAUNCH STAGES |
| 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 16127:2014 | Space systems — Prevention of break-up of unmanned spacecraft |
| ISO 24113:2011 | Space systems Space debris mitigation requirements |
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