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Aerospace isogrid structures include payload shrouds and boosters, which must support the full weight of upper stages and payloads under high G loads. Their open configuration with a single, sealed sheet facing the outside makes them especially useful for propellant tanks for rockets, where sealing the propellant in, but allowing it to drain in ...
They are created and maintained by the Aerospace Industries Association (AIA). [1] The Federal Aviation Administration recognizes National Aerospace Standards as "traditional standards" for the purposes of parts approval. [2] The primary AIA committee responsible for developing standards is the National Aerospace Standards Committee (NASC).
Aerospace materials are materials, frequently metal alloys, that have either been developed for, or have come to prominence through their use for aerospace purposes. These uses often require exceptional performance, strength or heat resistance, even at the cost of considerable expense in their production or machining.
Material selection is a step in the process of designing any physical object. In the context of product design, the main goal of material selection is to minimize cost while meeting product performance goals. [1] Systematic selection of the best material for a given application begins with properties and costs of
The new standardized document, called 9100, was still based on ISO 9001:1994(E), although it was published separately by each country's aerospace association or standards body (AS 9100 in the U.S). AS 9100 added 55 aerospace industry specific amplifications and requirements to ISO 9001:1994. [10]
S1000D is an international specification for the procurement and production of technical publications. It is an XML specification for preparing, managing, and publishing technical information for a product. It was initially developed by the AeroSpace and Defence Industries Association of Europe (ASD) for use with military aircraft.
ARP4754(), Aerospace Recommended Practice (ARP) Guidelines for Development of Civil Aircraft and Systems, is a published standard from SAE International, dealing with the development processes which support certification of Aircraft systems, addressing "the complete aircraft development cycle, from systems requirements through systems verification."
Specific modulus is a materials property consisting of the elastic modulus per mass density of a material. It is also known as the stiffness to weight ratio or specific stiffness. High specific modulus materials find wide application in aerospace applications where minimum structural weight is required.