ISO 10786:2011
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ISO 10786:2011
46099

Status : Published (To be revised)

This standard was last reviewed and confirmed in 2016. Therefore this version remains current.
This standard will be replaced by ISO/DIS 10786
en
Format Language
std 1 194 PDF
std 2 194 Paper
  • CHF194
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Abstract

ISO 10786:2011 establishes requirements for the design; material selection and characterization; fabrication; testing and inspection of all structural items in space systems, including expendable and reusable launch vehicles, satellites and their payloads. When implemented for a particular space system, it will assure high confidence in achieving safe and reliable operation in all phases of its planned mission.

ISO 10786:2011 applies specifically to all structural items, including fracture-critical hardware used in space systems during all phases of the mission, with the following exceptions: adaptive structures, engines and thermal protection systems.

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General information

  •  : Published
     : 2011-07
    : International Standard to be revised [90.92]
  •  : 1
     : 65
  • ISO/TC 20/SC 14
    49.140 
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