SAE AIR744A

Aerospace Auxiliary Power Sources.

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Standard:
  • AIR744
  • Revision: A
Reaffirmed:
  • 2011-08-10
Revised:
  • 1992-07-01
Revision:
  • Historical. Access the latest revision: AIR744C
Issuing:
  • A-6c6 Power Sources Committee
Scope:

This SAE Aerospace Information Report (AIR) is a review of the general characteristics of power sources that may be used to provide secondary, auxiliary, or emergency power for use in aircraft, space vehicles, missiles, remotely piloted vehicles, air cushion vehicles, surface effect ships, or other vehicles in which aerospace technology is used.The information contained herein is intended for use in the selection of the power source most appropriate to the needs of a particular vehicle or system. The information may also be used in the preparation of a power source specification.Considerations for use in making a trade study and an evaluation of the several power sources are included. More detailed information relating to specific power sources is available in other SAE Aerospace Information Reports or in Aerospace Recommended Practices.

History:
StandardPublishedRevisionStatus
AIR744C2010-06-16LatestRevised
AIR744B1995-07-01HistoricalReaffirmed
AIR744A1992-07-01HistoricalReaffirmed
AIR7441964-04-01HistoricalIssued
AKA:
  • SAE AIR 744
Sector:
  • Aerospace
Topic:
  • Electrical, Electronics and Avionics
  • Fly-by-wire control systems
  • Electrical Systems
  • Electromagnetic compatibility
  • Sensors and Actuators
  • Hybrid power
  • Electric hybrid power
  • Fluid power systems
  • Hydraulic systems
  • Electrohydraulics
  • Hydraulic motors
  • Fuel pumps
  • Auxiliary power units
  • Safety
  • Tests and Testing
  • Missiles
  • Unmanned aerial vehicles

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