ISO 21347:2005
Current
The latest, up-to-date edition.
Space systems — Fracture and damage control
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
English, French
27-05-2005
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ISO 21347:2005 establishes general requirements for the application of fracture control technology to fracture critical items (FCIs) fabricated by metallic, non-metallic or composite materials. It also establishes mechanical damage control requirements for mechanical damage critical items (MDCIs) fabricated by composite materials. These requirements, when implemented on a particular space system, may assure a high level of confidence in achieving safe operation and mission success.
The requirements set forth in ISO 21347:2005 are the minimum fracture control and mechanical damage control requirements for FCIs and MDCIs in general space systems, including launch vehicles and spacecraft. With necessary modifications, these requirements may also be applicable to reusable launch vehicles (RLVs). ISO 21347:2005 is not applicable to the NASA Space Shuttle and its payloads or the International Space Station and its equipment since they already have a set of specific requirements suitable for their special applications.
ISO 21347:2005 is not applicable in processing detected defects.
| DevelopmentNote |
Supersedes ISO/DIS 21347 (05/2005)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| ISO 10786:2011 | Space systems — Structural components and assemblies |
| BS ISO 16127:2014 | Space systems. Prevention of break-up of unmanned spacecraft |
| 07/30146415 DC : DRAFT AUG 2007 | BS ISO 21648 - SPACE SYSTEMS - FLYWHEEL MODULE DESIGN AND TESTING |
| BS ISO 21648:2008 | Space systems. Flywheel module design and testing |
| BS ISO 10786:2011 | Space systems. Structural components and assemblies |
| BS ISO 24638:2008 | Space systems. Pressure components and pressure system integration |
| 10/30197714 DC : 0 | BS ISO 10786 - SPACE SYSTEMS - STRUCTURAL COMPONENTS AND ASSEMBLIES |
| ISO 21648:2008 | Space systems — Flywheel module design and testing |
| 12/30213836 DC : 0 | BS ISO 16127 - SPACE SYSTEMS - PREVENTION OF BREAK-UP OF UNMANNED SPACECRAFT |
| ISO 16127:2014 | Space systems — Prevention of break-up of unmanned spacecraft |
| 07/30146438 DC : 0 | BS ISO 24638 - SPACE SYSTEMS - PRESSURE COMPONENTS AND PRESSURE SYSTEM INTEGRATION |
| ISO 24638:2008 | Space systems Pressure components and pressure system integration |
| ISO 14623:2003 | Space systems - Pressure vessels and pressurized structures — Design and operation |
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