BS ISO 16126:2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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. Assessment of survivability of unmanned spacecraft against space debris and meteoroid impacts to ensure successful post-mission disposal
Hardcopy , PDF
English
30-04-2014
04-12-2024
Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Abbreviated terms
5 Impact survivability assessment requirements
6 Impact survivability assessment procedure
7 Procedure for performing a simple impact
risk analysis
8 Procedure for performing a detailed impact
risk analysis
Annex A (informative) - Supplementary information
on the simple impact risk analysis procedure
Annex B (informative) - Ballistic limit equations
Annex C (informative) - Background information
on hypervelocity impact testing and modelling
Annex D (informative) - Method to calculate
impact-induced Probability of No Failure
Annex E (informative) - Options for improving
impact survivability
Bibliography
Specifies requirements and a procedure for assessing the survivability of an unmanned spacecraft against space debris and meteoroid impacts to ensure the survival of critical components required to perform post-mission disposal.
| Committee |
ACE/68
|
| DevelopmentNote |
Supersedes 12/30213833 DC. (04/2014)
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This International Standard defines requirements and a procedure for assessing the survivability of an unmanned spacecraft against space debris and meteoroid impacts to ensure the survival of critical components required to perform post-mission disposal. This International Standard also describes two impact risk analysis procedures that can be used to satisfy the requirements. The procedures are consistent with those defined in References [1] and [2].
This International Standard is part of a set of International Standards that collectively aim to reduce the growth of space debris by ensuring that spacecraft are designed, operated, and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime. All of the primary debris mitigation requirements are contained in a top-level International Standard.[3] The remaining International Standards, of which this is one, provide methods and processes to enable compliance with the primary requirements.
| Standards | Relationship |
| ISO 16126:2014 | Identical |
| ISO 14200:2012 | Space environment (natural and artificial) — Guide to process-based implementation of meteoroid and debris environmental models (orbital altitudes below GEO + 2 000 km) |
| ISO 10795:2011 | Space systems — Programme management and quality — Vocabulary |
| ISO 24113:2011 | Space systems — Space debris mitigation requirements |
| NSS 1740.14 : 0 | ORBITAL DEBRIS MANUAL |
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