SAE International Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of AS1831A

Description
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.
Description
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.

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Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of - AS1831A - SAE International
Warrendale, PA, United States
Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of
AS1831A
Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of 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.

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.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number AS1831A
Product Name Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of
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