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Standard

ELECTRIC POWER, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF

1971-12-01
HISTORICAL
AS1212
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.
Standard

Document for 270 Voltage Direct Current (270 V DC) System

2017-11-30
CURRENT
ARP4729A
This SAE Aerospace Recommended Practice (ARP) provides technical design and application information related to the generation, distribution, control, and utilization of aircraft 270 V DC electrical power systems and support equipment. This document also provides references and definitions to permit comparisons of various electrical systems and components.
Standard

DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM

1992-09-18
HISTORICAL
ARP4729
This SAE Aerospace Recommended Practice (ARP) provides technical design and application information related to the generation, distribution, control, and utilization of aircraft 270 V DC electrical power systems and support equipment. This document also provides references and definitions to permit comparisons of various electrical systems and components.
Standard

Space Power Standard

2012-04-11
HISTORICAL
AS5698
This standard defines the requirements and characteristics of electrical power for spacecraft. This standard also defines analysis, verification, and testing methodologies to be used to ensure that the loads operate when connected to the specified power quality and performance as defined by this standard.
Standard

Space Power Standard

2018-09-13
CURRENT
AS5698A
This standard defines the requirements and characteristics of electrical power for spacecraft. This standard also defines analysis, verification, and testing methodologies to be used to ensure that the loads operate when connected to the specified power quality and performance as defined by this standard.
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