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ISO 16126:2014

Current

Current

The latest, up-to-date edition.

Space systems — Assessment of survivability of unmanned spacecraft against space debris and meteoroid impacts to ensure successful post-mission disposal

Available format(s)

Hardcopy , PDF 1 User , PDF 3 Users , PDF 5 Users , PDF 9 Users

Language(s)

English, Russian

Published date

24-03-2014

ISO 16126:2014 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. ISO 16126:2014 also describes two impact risk analysis procedures that can be used to satisfy the requirements.

ISO 16126:2014 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.

Committee
ISO/TC 20/SC 14
DevelopmentNote
Supersedes ISO/DIS 16126. (03/2014)
DocumentType
Standard
Pages
19
PublisherName
International Organization for Standardization
Status
Current

Standards Relationship
BS ISO 16126:2014 Identical

ISO/TR 20590:2017 Space systems - Debris mitigation design and operation manual for launch vehicle orbital stages
PD ISO/TR 18146:2015 Space systems. Space debris mitigation design and operation guidelines for spacecraft
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 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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