SAE AS 1831 : 2010
SAE AS 1831 : 2010
ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF
SAE International
ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF
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.
Document Type | Standard |
Status | Current |
Publisher | SAE International |
Committee | AE-7C |