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  • SAE AIR 744 : 2015

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    AEROSPACE AUXILIARY POWER SOURCES

    Available format(s):  Hardcopy, PDF

    Superseded date:  24-11-2020

    Language(s):  English

    Published date:  26-10-2015

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. REFERENCES
    3. TYPES OF POWER SOURCES
    4. REQUIREMENTS FOR POWER SOURCES
    5. SOLID PROPELLANTS
    6. LIQUID PROPELLANTS
    7. HIGH PRESSURE STORED GAS SYSTEM
    8. ENGINE BLEED SYSTEMS
    9. RAM AIR TURBINES
    10. BATTERIES
    11. FUEL CELLS
    12. SOLAR CELLS
    13. NUCLEAR POWER SYSTEMS
    14. GAS TURBINE AUXILIARY POWER UNITS (APUS)
    15. FLYWHEELS
    16. NOTES

    Abstract - (Show below) - (Hide below)

    Specifies 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.

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    Committee A-6C4
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    SAE ARP 699 : 2015 HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT
    CFR 49(PTS400-571) : OCT 2017 TRANSPORTATION
    SAE J 1775 : 2015 BLEED-AIR PNEUMATIC SYSTEMS FOR GAS TURBINE EQUIPPED MARINE AND AMPHIBIOUS CRAFT
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    MIL-DTL-5624 Revision W:2016 TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5
    SAE AIR 1168/1 : 1990 THERMODYNAMICS OF INCOMPRESSIBLE AND COMPRESSIBLE FLUID FLOW
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL-PRF-7808 Revision L:1997 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    ASTM D 910 : 2017-05 SPECIFICATION FOR LEADED AVIATION GASOLINES
    SAE AIR 1343 : 2013 LIQUID PROPELLANT GAS GENERATION SYSTEMS
    MIL-PRF-23699 Revision G:2014 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE, NATO CODE NUMBERS: O-152, O-154, O-156, AND O-167
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