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SAE AS 1831 : 2010

SAE AS 1831 : 2010

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

SAE International

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Table of Contents

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

Abstract

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.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee AE-7C

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