This aerospace specification defines the requirements for metric weld fittings and machine weldments using an orbiting welding head suitable for use on cold worked 3A1-2.5V titanium and 21Cr-6Ni-9Mn CRES tubing and associated fittings. This specification is equivalent to AS1576 except for metric dimensions and standards.
This document establishes the temperature types and pressure classes that are commonly used in aerospace fluid systems. The temperature types and pressure classes are equivalent, but not identical, to the SI units defined in MA2001 (ISO 6771). For exact conversion use NAS 10000.
This document establishes the temperature types and pressure classes that are commonly used in aerospace fluid systems. The temperature types and pressure classes are equivalent, but not identical, to the SI units defined in MA2001 (ISO 6771). For exact conversion use NAS 10000.
This document describes the materials, equipment, and processing techniques used in fabricating high-strength or high-modulus graphite-fiber-reinforced polysulfone laminates for structural applications for service up to 120°C (250°F).
This document describes the materials, equipment, and processing techniques used in fabricating high-strength or high-modulus carbon-fiber-reinforced polysulfone laminates for structural applications for service up to 120°C (250°F).
This supplement forms a part of the Aerospace Standard AS5420, Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification, and shall be used to identify hose assembly standards citing this procurement specification.