Results
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
This SAE Aerospace Recommended Practice (ARP) establishes the overall component and system function guidelines and minimum performance levels for a TPMS. These guidelines include, but are not limited to: Design recommendations for system components, which: Monitor tire inflation Are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment Recommended performance and safety guidelines for a TPMS.
This specification covers a corrosion-resistant steel in the form of wire.
The following schematic diagrams reflect various methods of illustrating automotive transmission arrangements. These have been developed to facilitate a clear understanding of the functional interrelations of the gearing, clutches, hydrodynamic drive unit, and other transmission components. Two variations of transmission diagrams are used: in neutral (clutches not applied) and in gear. For illustrative purposes, some typical transmissions are shown.
This specification covers a columbium (niobium) alloy in the form of bars, rods, and extrusions.
This specification covers a corrosion- and heat-resistant steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
This specification covers one type of epoxy-resin-impregnated, non-woven, glass fiber in the form of tape for hand or machine layup and of flat sheet.
This specification covers one type of nickel-aluminum bronze in the form of extruded bars, rods, and tubes.
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and stock for forging or flash-welded rings.
This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides (thickness).
This specification covers a corrosion- and heat-resistant iron alloy in the form of welding wire.
This SAE Metric Aerospace Standard defines the requirements for corrosion resistant steel helical coil metric series screw thread inserts made from formed wire, the inner surfaces of which, after assembly, provide internal threads of the diameter and pitch specified on the drawing.
This specification covers an aluminum alloy in the form of sand, permanent mold, composite mold, and investment castings.
This specification covers the specific requirements for aluminum alloy 2014 bar, rod, shapes, tube, and wire produced by extrusion.
This specification covers an aluminum bronze alloy in the form of sand castings (see 8.5).
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing, flash-welded rings fabricated from extruded stock, and stock for flash-welded rings (see 8.6).
The scope of this SAE Aerospace Standard (AS) is to define the following dimensional requirements for double hexagon, hexagon head and tee headed bolts, and nuts with AS8879 UNJ inch series threads primarily for use in propulsion systems. Design requirements are based on UNJC threads for sizes 0.1640 and smaller and UNJF threads for sizes 0.1900 and larger.
This specification covers a thickened, water-base, type cleaner in the form of a gel.
This document specifies the procedure and requirements for gas nitriding steel parts by the use of raw or dissociated ammonia.
This specification covers an aluminum alloy in the form of extruded or drawn welding wire.
This report is limited to the special problems of air quantity, purity, movement, pressure, temperature, and humidity which arise from the requirements of the human body during high altitude flight, together with the associated aircraft design problems.
This aerospace recommended practice includes the type of lubricant to be used, conditions of lubrication, and torque-tension relationship of lock nut and bolts as required for desired preload.
This standard describes test methods for insulated, single conductor, electric wire intended for aerospace applications. Particular requirements for the wire being tested need to be specified in a procurement document or other detail specification. Suggested minimum requirements are included in the notes at the end of some of the test methods. SAE Performance Standard AS4372 uses some of the tests in this document for evaluating comparative performance of aerospace wires.
Items per page:
50
1 – 50 of 219518