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ISO 24638

Space systems - Pressure components and pressure system integration

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Organization: ISO
Publication Date: 15 November 2008
Status: active
Page Count: 32
ICS Code (Space systems and operations): 49.140
scope:

This International Standard 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.

This International Standard 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.

The requirements for pressure vessels and pressurized structures are set forth in ISO 14623.

This International Standard does not apply to engine components.

Document History

May 1, 2021
Space systems — Pressure components and pressure system integration
This document establishes the baseline requirements for the design, fabrication and testing of space flight pressure components. It also establishes the requirements for the assembly, installation,...
ISO 24638
November 15, 2008
Space systems - Pressure components and pressure system integration
This International Standard establishes the baseline requirements for the design, fabrication and testing of space flight pressure components. It also establishes the requirements for assembly,...

References

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