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.
Status: PublishedPublication date: 2014-04
Edition: 1Number of pages: 19
Technical Committee: ISO/TC 20/SC 14 Space systems and operations
Buy this standard
|std 1 124||PDF + ePub|
|std 2 124||Paper|
|std 3 124|