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
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Status: Under developmentStage: DIS registered [40.00]
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Edition: 2
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Technical Committee :ISO/TC 20/SC 14
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Life cycle
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Previously
PublishedISO 10786:2011
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