SAE AS 1831 : 2010

Superseded

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ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF

Available format(s)

Hardcopy , PDF

Superseded date

11-08-2020

Language(s)

English

Published date

01-01-2010

Publisher

SAE International

1. SCOPE
2. REFERENCES
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. DETAILED REQUIREMENTS - AIRCRAFT ELECTRICAL
POWER SYSTEM
6. LOAD DEMAND CONSTRAINTS
7. GROUND SUPPORT EQUIPMENT CHARACTERISTICS

Sets up 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.

Committee	AE-7C
DocumentType	Standard
Pages	12
PublisherName	SAE International
Status	Superseded
SupersededBy	SAE AS 1831A : 1997(R2017)
Supersedes	SAE AS 1831 : 1997

SAE ARP 4729 : 1992

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

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SAE AS 1831 : 2010

Superseded

Table of Contents

Abstract

General Product Information

Standards Referencing This Book

Category

Subcategory

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