Abstract
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.
General information
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Status: PublishedPublication date: 2014-04Stage: International Standard to be revised [90.92]
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Edition: 1Number of pages: 19
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Technical Committee :ISO/TC 20/SC 14ICS :49.140
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Life cycle
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Now
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Will be replaced by
Under developmentISO/FDIS 16126