ISO-10786 › Space systems - Structural components and assemblies

ISO-10786 - 1ST EDITION - CURRENT


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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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49.140 (Space systems and operations Including space data and information transfer systems, and ground support equipment for launch site operations)

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Document Number

ISO 10786:2011

Revision Level

1ST EDITION

Status

Current

Publication Date

July 15, 2011

Committee Number

ISO/TC 20/SC 14