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Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of
- Aerospace Standard
- AS1831A
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Scope
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.
Rationale
AS1831A has been reaffirmed to comply with the SAE Five-Year Review policy.
Recommended Content
Aerospace Standard | Document for 270 Voltage Direct Current (270 V DC) System |
Technical Paper | Generation and Suppression of Voltage Transients in Military Vehicular Electrical Systems |
Aerospace Standard | Electric Power, Aircraft, Characteristics and Utilization of |
Topic
Data Sets - Support Documents
No Datasets Available
Issuing Committee
The scope of the AE-7 Aerospace Electrical Power and Equipment Committee is dedicated to developing standards and specifications relative to the generation and control, storage, conversion, distribution, load management and utilization of electric power for aerospace vehicles. The Committee also provides a forum for gathering and disseminating electrical power and technical equipment information between users and suppliers.
Reference
Number | Title |
---|---|
ARP4729 | DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM |
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