ISO 24638:2008
Withdrawn
View Superseded by
Space systems — Pressure components and pressure system integration
Hardcopy , PDF
English
11-05-2008
04-09-2025
ISO 24638:2008 establishes the baseline requirements for the design, fabrication and testing of space flight pressure components. It also establishes the requirements for assembly, installation, test, inspection, operation and maintenance of the pressure systems in spacecraft and launch vehicles. These requirements, when implemented on a particular space system, ensure a high level of confidence in achieving safe and reliable operation.
ISO 24638:2008 applies to all pressure components other than pressure vessels and pressurized structures in a pressure system. It covers lines, fittings, valves, bellows, hoses and other appropriate components that are integrated to form a pressure system.
| DevelopmentNote |
Supersedes ISO/DIS 24638. (11/2008)
|
| DocumentType |
Standard
|
| Pages |
25
|
| PublisherName |
International Organization for Standardization
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| BS ISO 24638:2008 | Identical |
| BS ISO 16127:2014 | Space systems. Prevention of break-up of unmanned spacecraft |
| ISO 10786:2011 | Space systems — Structural components and assemblies |
| BS ISO 10786:2011 | Space systems. Structural components and assemblies |
| 10/30197714 DC : 0 | BS ISO 10786 - SPACE SYSTEMS - STRUCTURAL COMPONENTS AND ASSEMBLIES |
| 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 |
| ISO 21347:2005 | Space systems — Fracture and damage control |
| ISO 14623:2003 | Space systems - Pressure vessels and pressurized structures — Design and operation |
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