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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

Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of

2023-04-03
CURRENT
AS1831A
This SAE Aerospace Standard (AS) establishes the characteristics and utilization of 270 V DC electric power at the utilization equipment interface and the constraints of the utilization equipment based on practical experience. These characteristics shall be applicable for both airborne and ground support power systems. This document also defines the related distribution and installation considerations. Utilization equipment designed for a specific application may not deviate from these requirements without the approval of the procuring activity.
Standard

ELECTRICAL POWER, HIGH VOLTAGE DIRECT CURRENT, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF

1987-06-01
HISTORICAL
AS1831
This standard establishes the characteristics and utilization of 270-VDC electric power at the utilization equipment interface and the constraints on the utilization equipment. These characteristics shall be applicable for both airborne and ground support power systems. This standard also defines the related distribution and installation considerations. Utilization equipment designed for a specific aircraft application may not deviate from these requirements without the approval of the procuring activity.
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.
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.
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