ISO 10786:2011
Current
The latest, up-to-date edition.
Space systems — Structural components and assemblies
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English
08-07-2011
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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.
| DevelopmentNote |
Supersedes ISO/DIS 10786. (07/2011)
|
| DocumentType |
Standard
|
| Pages |
65
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| Standards | Relationship |
| BS ISO 10786:2011 | Identical |
| AIAA S 110 : 2005 | SPACE SYSTEMS - STRUCTURES, STRUCTURAL COMPONENTS, AND STRUCTURAL ASSEMBLIES |
| ISO 14954:2005 | Space systems — Dynamic and static analysis — Exchange of mathematical models |
| ISO 24638:2008 | Space systems Pressure components and pressure system integration |
| MIL-STD-1540 Revision D:1999 | TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES |
| DOT/FAA/AR-MMPDS-01 : 20030131 | METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS) |
| ASTM E 740 : 2003 | Standard Practice for Fracture Testing with Surface-Crack Tension Specimens |
| ISO 21347:2005 | Space systems — Fracture and damage control |
| ISO 16454:2007 | Space systems — Structural design — Stress analysis requirements |
| ISO 21648:2008 | Space systems — Flywheel module design and testing |
| ISO 15864:2004 | Space systems General test methods for space craft, subsystems and units |
| ISO 22010:2007 | Space systems — Mass properties control |
| ISO 24917:2010 | Space systems General test requirements for launch vehicles |
| ISO 14623:2003 | Space systems - Pressure vessels and pressurized structures — Design and operation |
| ISO 14953:2000 | Space systems — Structural design — Determination of loading levels for static qualification testing of launch vehicles |
| ISO 14622:2000 | Space systems — Structural design — Loads and induced environment |
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