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BS 1771-1 covers fabric details
The reason for the standardization of the drawing elements for these types of symbols is to ensure uniformity and legibility when they are reduced in size to fit on a control button or panel
• Interface between traction system and auxiliary power supply system
3 Leak test on minimum and maximum pressures of compressed air for pneumatic valve
Space systems. Structural components and assemblies Ingestion-build-82396 BS 1771-1 covers fabric details1 Scope This International Standard 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. This International Standard, when implemented for a particular space system, will assure high confidence in achieving safe and reliable operation in all phases of its planned
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