Space systems. Pressure components and pressure system integration Ingestion-build-48068

Space systems. Pressure components and pressure system integration Ingestion-build-48068BS ISO 24638: 2008 Space systems. Pressure components and pressure system integration BS ISO 24638 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

7 Electrical interfaces

issuance and operation of arrangements for the recognition and acceptance of results produced by bodies undertaking similar conformity assessment and related activities

references were updated and the document was editorially revised

which cancels and replaces ISO 3951-1:2006 and is a minor revision of that standard with the following changes:

If no European methods exist

Reference to the latest version of EN 60068-2-47: Mounting

the body size of the intended wearer has to be defined and identified with the nearest size on a table of standard sizes

As per BS 6349-2

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Leather is a strong and flexible material to be used

BS EN IEC 60721-2-4:2018 will assist product designers in evaluating the effects of solar radiation on the products in service both in terms of the n of physical properties of materials and the effects of solar heating and the operating temperatures attained as a result

This standard replaces BS EN 61131-3:2003