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This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
This SAE Recommended Practice covers equipment capabilities and the test procedure to quantify and qualify the shear strength between the friction material and backing plate or brake shoe for automotive applications. This SAE Recommended Practice is applicable to: bonded drum brake linings; integrally molded disc brake pads; disc brake pads and backing plate assemblies using mechanical retention systems (MRS); coupons from drum brake shoes or disc brake pad assemblies. The test and its results are also useful for short, semi-quantitative verification of the bonding and molding process. This Recommended Practice is applicable during product and process development, product verification and quality control. This Recommended Practice does not replicate or predict actual vehicle performance or part durability.
Brake Linings Standards Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
The scope of this information report applies to the steady state measurement of direct mass fuel flow in gas turbine engine test cells. A measurement accuracy, and hence uncertainty of between ±0.1 to ±0.2% of value is believed to be achievable for liquid flow applications with some meter models/installations. Whilst capable of general transient measurement in 50 to 100 Hz region, this type of fuel meter is not capable of rapid transient measurement (in 100 to 250 Hz region). It is also not currently considered suitable for "in flight" fuel flow measurement.
EG-1E Gas Turbine Test Facilities and Equipment
This guide provides implementation consideration guidance for the normative clauses of IEEE/EIA 12207.0. The guidance is based on software industry experience with the life cycle processes presented in IEEE/EIA 12207.0.
Systems Management Council
This standard is applicable to the engineering or the reengineering of: a Commercial or non-commercial systems, or portions thereof; b Any system, small or large, simple or complex, software-intensive or not, precedented or unprecedented; c Systems made up of hardware, software, firmware, personnel, facilities, data, materials, services, techniques, or processes (or combinations thereof); d A new system or a legacy system, or portions thereof. The requirements of this standard, or a designated subset, are intended to be applied by projects establishing policies and procedures for project implementation of the adopted process and process elements of this standard. The requirements of this standard may be tailored as follows: a Processes – Processes may be tailored to be applicable for a given type of project or system. For example, the System Utilization Processes typically don’t apply for conceptual or prototype systems in the same manner as for full-volume production systems. b
G-47 Systems Engineering
This Aerospace Recommended Practice (ARP) provides guidance for the design of an integrated vehicle health management (IVHM) capability that will extend the vehicle’s inherent design to enable health management of the platform and its components. This guidance is technology-independent; the principles are generally applicable to the majority of potential IVHM design scenarios, including “clean sheet” system design, where IVHM is considered as a primary design consideration, and the retrofit design, where existing systems are modified and leveraged with the IVHM capability. In either case, this ARP provides guidance for designing the IVHM capability from the feasibility assessment to the conceptual design analysis and to the development design phases, with considerations given to trade studies, metrics, and life cycle impacts.
HM-1 Integrated Vehicle Health Management Committee
This standard establishes requirements when implementing statistical product acceptance methods to meet defined risk requirements. This standard also establishes the minimum content required to be covered in an organization’s documented procedures that govern their application of statistical product acceptance methods. These general requirements and documented procedures apply the requirements of the 9100/9110/9120 quality management system standards, in addition to establishing requirements for retrievability, safety/critical characteristics, and quality parameters that protect the customer.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry.
Engine Power Test Code Committee
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.
AMS P17 Polymer Matrix Composites Committee
This specification covers an aluminum or aluminum alloy in the form of sheet, laminated and edge bonded.
AMS D Nonferrous Alloys Committee
This specification covers cabled-strand ropes formed from impregnated aramid fibers.
AMS P Polymeric Materials Committee
This specification covers a high-carbon steel in the form of bars.
AMS E Carbon and Low Alloy Steels Committee
This specification covers pure gold in the form of wire 0.005 to 0.040 inch (0.012 to 1.000 mm) inclusive, in nominal diameter, and ribbon 0.002 to 0.051 inch (0.05 to 1.28 mm) inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers one type of parchment in the form of rolls of sheeting or reels of unperforated tape of the width specified.
AMS P17 Polymer Matrix Composites Committee
This specification covers one type of epoxy-resin-impregnated boron filaments 0.0040 inch (0.102 mm) in diameter in the form of continuous tape supported on a glass cloth carrier.
AMS P17 Polymer Matrix Composites Committee
This specification covers an aluminum-killed carbon steel in the form of sheet and strip.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a cobalt alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers three classes of para-aramid tape and webbing of a single width and with varying weights.
AMS P Polymeric Materials Committee
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.
AMS P17 Polymer Matrix Composites Committee
This specification covers a silicone rubber sponge in the form of sheet, strip, extrusions, and molded shapes.
AMS CE Elastomers Committee
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
AMS P17 Polymer Matrix Composites Committee
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.
AMS P17 Polymer Matrix Composites Committee
This specification covers one weight and one weave of nylon cloth.
AMS P Polymeric Materials Committee
This specification covers a palladium-silver alloy in the form of round wire 0.004 to 0.080 inch (0.10 to 2.03 mm) inclusive, in nominal diameter (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers one strength and weight of nylon fabric in the form of webbing.
AMS P Polymeric Materials Committee
This specification covers a polyalphaolefin/ester-blend fluid.
AMS CE Elastomers Committee
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.
AMS P17 Polymer Matrix Composites Committee
This specification covers four classes of para-aramid tape and webbing of a single width and with varying weights.
AMS P Polymeric Materials Committee
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
AMS P17 Polymer Matrix Composites Committee
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.
AMS P17 Polymer Matrix Composites Committee
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
AMS P17 Polymer Matrix Composites Committee
This specification covers a denatured ethyl alcohol in the form of a liquid.
AMS B Finishes Processes and Fluids Committee
This specification covers a petroleum-base liquid solvent.
AMS B Finishes Processes and Fluids Committee
In 1941, the SAE Iron and Steel Division in collaboration with the American Iron and Steel Institute (AISI) made a major change in the method of expressing composition ranges for the SAE steels. The plan, as now applied, is based in general on narrower ladle analysis ranges plus certain product (check) analysis allowances on individual samples, in place of the fixed ranges and limits without tolerances formerly provided for carbon and other elements in SAE steels (reference SAE J408). ISTC Division 1 has developed a procedure which allows for the maintenance of the grade list in this SAE Standard. This will involve conducting an industry-wide survey to solicit input. This survey will be conducted at a frequency deemed necessary by the technical committee. Criteria have been established for the addition to or deletion of grades from the grade table. A new grade will be considered if it meets standard SAE grade ranges, has a minimum usage or production of 225 tonnes/year (250 tons/year
Metals Technical Committee
This specification covers one width and strength of nylon tape.
AMS P Polymeric Materials Committee
This specification covers one class of para-aramid tape and webbing of a single width and with varying weights.
AMS P Polymeric Materials Committee
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