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CURRENT
2016-09-15
Standard
AMS2232H
This specification covers established inch/pound manufacturing tolerances applicable to carbon steel sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term “excl” is used to apply only to the higher figure of the specified range. Tolerances for product sizes not listed herein shall be as agreed upon by purchaser and vendor.
CURRENT
2016-09-15
Standard
CPGM1_17LT4CAMA
This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.
CURRENT
2016-09-15
Standard
CPGM2_17LT4CAMA
This product includes information on the manufacturer, engine, applications, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds. In addition, this product contains complete engine information such as displacement, cylinder configuration, valve train, combustion cycle, pressure charging, charge air cooling, bore, stroke, cylinder numbering convention, firing order, compression ratio, fuel system, fuel system pressure, ignition system, knock control, intake manifold, exhaust manifold, cooling system, coolant liquid, thermostat, cooling fan, lubricating oil, fuel, fuel shut off speed, etc. Also included are all measured test parameters outlined in J2723.
CURRENT
2016-09-14
Standard
AMS3894/1C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
CURRENT
2016-09-14
Standard
AMS3894/18A
This specification covers one type of toughened, high-impact epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
CURRENT
2016-09-14
Standard
AMS3894/3C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
CURRENT
2016-09-14
Standard
AMS3894/2C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
CURRENT
2016-09-14
Standard
AMS3894/7C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
CURRENT
2016-09-14
Standard
AMS3894/5C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
CURRENT
2016-09-14
Standard
AMS3894/9C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
2016-09-14
WIP Standard
GA-D16AA
This General Agreement presents default casting acceptance criteria for those casting specifications which do not explicitly contain criteria concerning flaws located close to the edge.
2016-09-14
WIP Standard
AS50861B
This specification covers polyvinyl chloride insulated single conductor electric wires made with tincoated copper conductors or silver-coated copper alloy conductors as specified in the applicable detail specification. The polyvinyl chloride insulation of these wires may be used alone or in combination with other insulating or protective materials.
2016-09-14
WIP Standard
AS81044B
This specification covers single conductor electric wires made as specified in the applicable specification sheet with tin-coated, silver-coated, or nickel-coated copper or copper alloy conductors insulated with crosslinked polyalkene, crosslinked alkane-imide polymer, or polyarylene. The crosslinked polyalkene, crosslinked alkane-imide polymer, or polyarylene may be used alone or in combination with other insulation materials as specified in the specification sheet.
2016-09-14
WIP Standard
J257
The minimum performance values in this SAE Recommended Practice are applicable to vehicles with brake systems having typical service pressure ranges 0 to 16.6 MPa (0 to 2400 psi) hydraulic or 0 to 945 kPa (0 to 135 psi) air only. SAE J880 not only provides for determining maximum brake rating power capability, but also permits verification of any desired or arbitrary level such as the requirement established herein. The determining criteria for deciding brake rating power capability are: a. Cold brake stopping ability. b. Fade as a result of brake power absorption. c. Hot brake stopping ability following brake power absorption. d. Brake system stability following brake power absorption. e. Functional and structural integrity of brake system following test.
2016-09-14
WIP Standard
J2999
This SAE Standard provides a method for determining the Effective Projected Luminous Lens Area (EPLLA) of a lamp function using design analysis. This standard was created to clarify and address how to determine EPLLA with traditional and new technologies. Lamps can be evaluated using the method described in SAE J3333; however, no lamp is subjected to both methods.
2016-09-14
WIP Standard
AIR4886A
The purpose of this document is to establish the requirements for Real-Time Communication Protocols (RTCP). Systems for real-time applications are characterized by the presence of hard deadlines where failure to meet a deadline must be considered a system fault. These requirements have been drive predominantly, but not exclusively, by aerospace type military platforms and commercial aircraft, but are generally applicable to any distributed, real-time, control systems. These requirements are primarily targeted for the Transport and Network Layers of peer to peer protocols, as referenced in the Open System Interconnect Reference Model (2.2.1 and 2.2.2), developed by the International Standards Organization (ISO). These requirements are intended to complement SAE AS4074 (2.1.1) and AS4075 (2.1.2), and future SAE communications standards.
2016-09-14
WIP Standard
AS15532A
The emphasis in this standard is the development of data word and message formats for AS15531 or MIL-STD-1553 data bus applications. This standard is intended as a guide for the designer to identify standard data words and messages for use in avionics systems and subsystems. These standard words and messages, as well as the doumentation format for interface control document (ICD) sheets, provide the basis for defining 15531/1553 systems. Also provided in this standard is the method for developing additional data word formats and messages that may be required by a particular system but are not covered by the formats provided herein. It is essential that any new word formats or message formats that are developed for a 15531/1553 application follow the fundamental guidelines estalbished in this standard in order to ease future standardization of these words an messages. The standard word formats presented represent a composite result of studies conducted by the U.S.
2016-09-14
WIP Standard
AMS4315A
This specification covers an aluminum alloy in the form of sheet and plate.
2016-09-14
WIP Standard
AMS4335A
This specification establishes requirements for 2xxx-series and 7xxx- series aluminum alloy forgings of any shape or form from which finished parts are to be made.

These forgings are used typically in the manufacture of high-performance parts when control of short-transverse tensile properties and fracture toughness is required, but usage is not limited to such applications.

2016-09-14
WIP Standard
AMS4434N
This specification covers a magnesium alloy in the form of sand castings.
2016-09-14
WIP Standard
AMS4443H
This specification covers a magnesium alloy in the form of sand castings.
2016-09-14
WIP Standard
AMS4472A
This specification covers an aluminum alloy in the form of plate.
2016-09-14
WIP Standard
AMS2399B
This specification covers the engineering requirements for electroless deposition of nickel-boron on various materials and the properties of the deposit.
2016-09-14
WIP Standard
AMS2434E
This specification covers the requirements for the electrodeposited tin-zinc alloy plating.
2016-09-14
WIP Standard
AMS2433D
This specification covers the requirements for an electroless nickel-thallium-boron or nickel-boron deposit on various substrates.
2016-09-14
WIP Standard
AMS2444B
This specification covers the requirements for the application and properties of a titanium nitride coating on metal parts applied by physical vapor deposition (PVD).
2016-09-14
WIP Standard
AS4074B
This standard specifies the characteristics of the SAE Linear Token Passing Bus (LTPB) Interface Unit. The LTPB provides a high reliability, high bandwidth, low latency serial interconnection network suitable for utilization in real time military and commercial applications. Multiple redundant data paths can be implemented to enhance reliability and survivability in those applications which require these attributes. The token passing and data exchange protocols are optimized to provide low latency and fast failure detection and correction. Physical configurations with bus lengths up to 1000 m can be accommodated.
2016-09-14
WIP Standard
AIR4271A
This Aerospace Information Report (AIR) has been prepared by the Systems Applications and Requirements Subcommittee of SAE Committee AS-2. It is intended to provide guidance primarily, but not exclusively, for specifiers and designers of data communication systems for real time military avionics applications within a platform. The subject of high speed data transmission is addressed from two standpoints 1) the influence of developments in technology on avionics architectures as a whole and 2) the way in which specific problems, such as video, voice, closed loop control, and security may be handled. While the material has been prepared against a background of experience within SAE AS-2 relating to the development of a family of high speed interconnect standards, reference to specific standards and interconnect systems is minimized.
2016-09-14
WIP Standard
AS4074/2B
This slash sheet specifies the operational parameters and characteristics of a particular implementation of the SAE Linear, Token Passing Bus (LTPB) Interface Unit. This slash sheet defines the following: a. the physical media interface: this slash sheet specifies the characteristics of the optical interface to the physical bus media; b. the minimum and maximum timing requirements for operation of this implementation of the LTPB; c. the data coding used to encode and decode the data for transmission; and d. the default values to be loaded into the timers of the LTPB interface at power-up prior to intervention by the host processor.
2016-09-14
WIP Standard
AIR5683A
MIL-STD-1553 establishes requirements for digital command/response time division multiplexing (TDM) techniques on military vehicles, especially aircraft. The existing MIL-STD-1553 network operates at a baud rate of 1 Mbps and is limited by the protocol to a maximum data payload capacity of approximately 700 kilobits per second. The limited capacity of MIL-STD-1553 buses coupled with emering data rich applications for avionics platforms plus the expense involved with changing or adding wires to thousands of aircraft in the fleet has driven the need for expanding the data carrying capacity of the existing MIL-STD-1553 infrastructure.
Viewing 61 to 90 of 43363