BS ISO 16164:2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Space systems. Disposal of satellites operating in or crossing Low Earth Orbit
Hardcopy , PDF
04-08-2022
English
31-07-2015
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Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Symbols and abbreviated terms
5 LEO protected region
6 Primary requirements
7 Disposal planning requirements
8 Disposal manoeuvre requirements
Annex A (informative) - Procedure to select a
post-mission disposal option
Annex B (informative) - Procedure for performing a
post-mission disposal manoeuvre
Bibliography
Defines requirements for the following: a) planning for disposal and passivation of spacecraft operating in LEO to ensure that final disposal is sufficiently characterized and that adequate propellant will be reserved for any propulsive manoeuvre required, b) selecting a disposal orbit where the spacecraft will re-enter the Earth's atmosphere within the next 25-years, or where the spacecraft will not re-enter the protected region within the next 100-years, and c) estimating, prior to launch, a 90% or better probability of successfully executing the disposal manoeuvre.
| Committee |
ACE/68
|
| DevelopmentNote |
Supersedes 14/30213848 DC. (07/2015)
|
| DocumentType |
Standard
|
| Pages |
22
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| ISO 16164:2015 | Identical |
| ISO 27875:2010 | Space systems Re-entry risk management for unmanned spacecraft and 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 |
| ISO 27852:2016 | Space systems — Estimation of orbit lifetime |
| ISO 23339:2010 | Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant |
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