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Viewing 31 to 60 of 5822
2017-06-08
WIP Standard
J2801
This SAE Standard applies to 12 V, flooded and absorptive glass mat lead acid automotive storage batteries of 200 minutes or less reserve capacity and cold crank capacity greater than 200 amperes. This life test is considered to be comprehensive in terms of battery manufacturing technology; applicable to lead-acid batteries containing wrought or cast positive grid manufacturing technology and providing a reasonable correlation for hot climate applications. This document is intended as a guide toward standard practice, but may be subject to change to keep pace with experience and technical advances.
CURRENT
2017-06-07
Standard
AS81659B
This specification covers two series of electrical, rectangular connectors with crimp type removable contacts. These connectors are provided with single, dual, triple, and quadruple insert shell configurations.
2017-06-05
WIP Standard
AS85049/150
This AS85049 product will accommodate the user demand for a re-positionable sealed shield termination backshell for suited applications.
2017-06-05
WIP Standard
AIR6808
This SAE Aerospace Information Report (AIR) is limited to the requirements of AS50881 and examines these requirements providing rationale behind them. SAE AS50881 is only applicable to the aircraft electrical wiring and interconnect system (EWIS). Pods and other devices that can be attached to an aircraft that are considered as aircraft equipment design. The AS50881 scope does not include attached devices, but does include the interface between the pod and aircraft wiring. Paragraph 3.3.5 addresses components such as antennas and other similar equipment that was once supplied as GFAE.
CURRENT
2017-06-01
Standard
AS81714/5A
SCOPE IS UNAVAILABLE.
2017-05-31
WIP Standard
AS81306A
This specification covers tools used to install tiedown straps on wire bundles and for installing connector accessory shield termination bands.
2017-05-26
WIP Standard
ARP6807
The intent of the SAE Recommended Practice (ARP) is to provide process for users to identify the part number of AS7928 terminal lugs installed in civilian or military applications, although can be used to identify terminals that have not been stored correctly. Thie ARP is subject to change to keep pace with experience and technical advances of AS7928 terminals. A current set of tables are provided to list and identify current AS7928 terminal lug configurations per the associated specification detail sheet and terminal lug configuration. Specific configuration details, graphic, size and marking information for each individual terminal lug is provided to assist the product user with accurate selection for replacement or identification.
2017-05-26
WIP Standard
AS31031B
SCOPE IS UNAVAILABLE.
CURRENT
2017-05-26
Standard
J2396_201705
This SAE Recommended Practice defines key terms used in the description and analysis of video based driver eye glance behavior, as well as guidance in the analysis of that data. The information provided in this practiced is intended to provide consistency for terms, definitions, and analysis techniques. This practice is to be used in laboratory, driving simulator, and on-road evaluations of how people drive, with particular emphasis on evaluating Driver Vehicle Interfaces (DVIs; e.g., in-vehicle multimedia systems, controls and displays). In terms of how such data are reduced, this version only concerns manual video-based techniques. However, even in its current form, the practice should be useful for describing the performance of automated sensors (eye trackers) and automated reduction (computer vision).
CURRENT
2017-05-26
Standard
J3117_201705
This document covers un-shielded balanced single twisted pair data cable intended for use in surface vehicle cables for 100 Mbps Ethernet applications. The tests in this document are intended to qualify cables for normal operation in an automotive environment while maintaining the necessary electrical properties for reliable data transmission.
CURRENT
2017-05-25
Standard
AS39029/90B
No scope available.
2017-05-25
WIP Standard
ARP1107C
This recommended practice covers the fixed structure, or independent energy absorbing system affixed to the airframe to afford protection to the control surfaces, engine and other portions during ground handling, take-off and landing.
2017-05-25
WIP Standard
J1113/27
1.1 Vehicle electrical/electronic systems may be affected when immersed in an electromagnetic field generated by sources such as radio and TV broadcast stations, radar and communication sites, mobile transmitters, cellular phones, etc. The reverberation method is used to evaluate the immunity of electronic devices in the frequency range of 500 MHz to 2.0 GHz, with possible extensions to 200 MHz and 10 GHz, depending upon chamber size and construction. Optional pulse modulation testing at HIRF (High Intensity Radiated Fields) test levels, based upon currently known environmental threats, has been added to this revision of the standard. This document addresses the Mode Stir (Continuous Stirring) Reverberation testing method which has been successfully utilized as a design and production stage development tool for many years.
2017-05-25
WIP Standard
J551/16
1.1 Vehicle electrical/electronic systems may be affected when immersed in an electromagnetic field generated by sources such as radio and TV broadcast stations, radar and communication sites, mobile transmitters, cellular phones, etc. This part of SAE J551 specifies off-vehicle radiated source test methods and procedures for testing passenger cars and commercial vehicles within a Reverberation Chamber. The method is used to evaluate the immunity of vehicle mounted electronic devices in the frequency range of 80 MHz to 2 GHz, with possible extensions 20 MHz to 10 GHz, depending upon chamber size and construction. Three methods for calibrating and applying electromagnetic fields are described in the document: 1) Mode Tuned Reverberation Chamber method, 2) Mode Stir (Standard) Reverberation Chamber method and 3) Mode Stir (Hybrid) Reverberation Chamber method.
CURRENT
2017-05-25
Standard
AS20708/131B
Scope is unavailable.
2017-05-23
WIP Standard
AS5680B
This interface standard applies to fuzes used in airborne weapons that use a 3-in fuze well. It defines: - Physical envelope of the fuze well at the interface with the fuze. - Load bearing surfaces of the fuze well. - Physical envelope of the fuze and its connector. - Mechanical features (e.g., clocking feature). - Connector type, size, location and orientation. - Retaining ring and its mechanical features (e.g., thread, tool interface). - Physical envelope of the retaining ring at the interface with the fuze. - Physical space available for installation tools. - Torque that the installation tool shall be capable of providing. This standard does not address: - Materials used or their properties. - Protective finish. - Physical environment of the weapon. - Explosive interface or features (e.g., insensitive munitions (IM) mitigation). - Charging tube. - Torque on the retaining ring or loads on the load bearing surfaces.
2017-05-23
WIP Standard
AS4270A
This document establishes techniques for validating that a mission store comples with the interface requirements delineated in MIL-STD-1760.
2017-05-23
WIP Standard
AIR6027A
The information presented in this AIR is intended to provide designers of armed unmanned systems with guidelines that may be applied to ensure safe integration and operation of weapons on unmanned platforms. The guidelines have been developed from experiences gained in the design and operation of weapons on manned aircraft that have been accepted by relevant safety authorities in the USA and Europe and proven effective over many years. Whilst the guidelines have been developed from experience with aircraft operations, the concepts are considered equally applicable to non-aircraft systems, such as those used on the surface or undersea environments.
2017-05-23
WIP Standard
AS47642B
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760C. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies. For validation of aircraft designed to MIL-STD-1760B Notice 3 AS47641 Issued 1999-08 applies.
2017-05-23
WIP Standard
AS4764A
This document establishes techniques for validating that an aircraft station complies with the interface requirements delineated in MIL-STD-1760.
2017-05-23
WIP Standard
AS47641A
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies.
2017-05-22
WIP Standard
AIR6540
The scope of this report is to capture the fundamental principles of selecting a wire size for an aerospace application using the method prescribed in SAE AS50881 standard. Also, provided in this report are additional calculations to ensure the wire selection will adequately perform in a particular design function including meeting environment constraints. Some of the calculations in this report have been simplified to demonstrate the process for validating the wire size selections for a particular design application. More precise calculations should be investigated and evaluated to ensure proper assessment of each individual calculation in this report.
CURRENT
2017-05-22
Standard
AS5259/8
AS5259/8 IS DESIGNED TO FUNCTION AS A REMOTE ELECTRICAL PUMP VERSION OF THE AS5259/4-01 OR THE AS5259/5-01 BASIC TOOLS MANUAL PUMP VERSIONS. CRIMPING IS LIMITED TO WIRE SIZES 8 THROUGH 2 FOR INSULATED TERMINALS AND 8 THROUGH 00 FOR UN-INSULATED TERMINALS AND CONTACTS (SEE TABLE 1).
CURRENT
2017-05-22
Standard
AS39029/91B
SCOPE IS UNAVAILABLE.
Viewing 31 to 60 of 5822