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2017-09-24
WIP Standard
ARP5584A
This SAE Aerospace Recommended Practices (ARP) covers the definitions, functions and broad application guidelines of modern aerospace vehicle electric power management systems. As aerospace control systems have become more sophisticated and autonomous, the electric power subsystem no longer is just a generation and distribution bus control system. New electric power systems include integration of individual load logic control, protection, generation, distribution, and load management. This system can report to a higher level control system, typically a vehicle management system, or can be an autonomous system within itself reporting and responding to operator commands.
CURRENT
2017-09-19
Standard
J2908_201709
This document provides test methods for evaluating the maximum power of electrified vehicle powertrain systems by direct measurement at the drive wheel hubs or axles. Additional tests are included specifically for PHEVs to measure electric-only propulsion power and for HEVs to measure electric power assist and regenerative braking. The testing requires either a chassis or hub dynamometer for all driven wheels. Results are processed to provide fair and consistent comparisons of power capabilities among different designs of electrified powertrains. Tests can also be performed on conventional vehicles if precise comparisons to electrified vehicles are desired.
2017-03-07
WIP Standard
AS81790B
This specification covers the requirements for aircraft external electric power receptacles.
CURRENT
2016-12-20
Standard
AS6349
This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary alternating current (AC) electrical power sources in aerospace electric power systems.
CURRENT
2014-06-13
Standard
AS5625A
This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary alternating current (AC) electrical power sources in aerospace electric power systems.
CURRENT
2014-03-31
Standard
USCAR4-1
This standard is intended to cover cigar or cigarette lighters as well as power outlets based on the form and dimensions of the cigar lighter. This standard is a full performance specification, it includes dimensional and operational parameters as well as performance characteristics which must be met when submitting a cigar lighter assembly or power outlet assembly for production approval. This standard constitutes an acceptance specification for a surface mounted, front-loaded cigar lighter or power outlet.
CURRENT
2012-12-05
Standard
AS1212A
The standard delineates the characteristics of electric power supplied to airborne equipment at the equipment terminals and the requirements for the utilization of such electric power by the airborne equipment.
CURRENT
2012-07-11
Standard
AS5663A
In lieu of TSO-C135, this SAE Aerospace Standard (AS) prescribes the minimum performance standards for wheels, brakes, and wheel and brake assemblies using electric power actuation for transport category (14 CFR Part 25) airplanes. Testing is limited to that necessary to establish minimum performance related to strength, robustness, stopping capability, and energy absorption to ensure measurable, repeatable industry accepted standards for these aspects of wheel and brake performance. The test parameters associated with electric braking actuation are defined around the state of the technology at this time, typically comprised of an Electro-Mechanical Actuator (EMA) controlled by a control system delivering electric power and effecting motor control.
2012-02-15
WIP Standard
J2997
To develop standards for a testing and identity regimen to define batteries for variable safe reuse. Utilize existing or in process standards such as Transportation, Labelling and State of Health.Add to these reference standardsthe required information to provide a safe and reliable usage.
CURRENT
2011-08-03
Standard
AS8023B
This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary alternating current (AC) electrical power sources in aerospace electric power systems.
CURRENT
2011-07-26
Standard
AS81790A
This specification covers the requirements for aircraft external electric power receptacles.
CURRENT
2011-07-21
Standard
AS4361A
This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary direct current (DC) electrical power sources in aerospace electric power systems. The purpose of this document is to define the guidelines and minimum performance test standards to be met by static electric power converters designed to operate from primary electric power systems. The tests specified herein provide a laboratory means to determine the performance and reliability characteristics of electric power converters under electrical and environmental conditions representative of these encountered in actual aerospace applications.
HISTORICAL
2009-11-18
Standard
AS81790_A3
This document has been taken directly from U.S. Military Specification MIL-C-81790A, Amendment 1 and contains only minor editorial and format changes required to bring it into conformance with the publishing requirements of SAE technical standards. The initial release of this document is intended to replace MIL-C-81790A, Amendment 1. Any part numbers established by the original specification remain unchanged. This specification covers the requirements for aircraft external electric power receptacles.
HISTORICAL
2007-09-05
Standard
AS81790_A2
Amendment 2 of AS81790.
HISTORICAL
2007-01-23
Standard
AS5663
In lieu of TSO-C135, this SAE Aerospace Standard (AS) prescribes the minimum performance standards for wheels, brakes, and wheel and brake assemblies using electric power actuation for transport category (14 CFR Part 25) airplanes. Testing is limited to that necessary to establish minimum performance related to strength, robustness, stopping capability, and energy absorption to ensure measurable, repeatable industry accepted standards for these aspects of wheel and brake performance. The test parameters associated with electric braking actuation are defined around the state of the technology at this time, typically comprised of an Electro-Mechanical Actuator (EMA) controlled by a control system delivering electric power and effecting motor control.
HISTORICAL
2007-01-18
Standard
AS5625
This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary alternating current (AC) electrical power sources in aerospace electric power systems.
HISTORICAL
2006-08-10
Standard
AS8023A
This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary alternating current (AC) electrical power sources in aerospace electric power systems.
HISTORICAL
2004-12-30
Standard
AS25486_A1
Amendment 1 of AS25486.
HISTORICAL
2004-09-01
Standard
AS90362_A1
Amendment 1 of AS90362.
HISTORICAL
2004-09-01
Standard
AS81790_A1
Amendment 1 of AS81790.
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