Draft
International Standard
ISO/DIS 10786
Space systems — Structural components and assemblies
Reference number
ISO/DIS 10786
Edition 2
Draft International Standard
Read sample
ISO/DIS 10786
85531
This Draft International Standard is in the enquiry phase with ISO members.
Will replace ISO 10786:2011

ISO/DIS 10786

ISO/DIS 10786
85531
Language
Format
CHF 63
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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.

General information

  •  : Under development
    : Full report circulated: DIS approved for registration as FDIS [40.99]
  •  : 2
     : 74
  • ISO/TC 20/SC 14
    49.140 
  • RSS updates

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