SAE AIR744C
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Aerospace Auxiliary Power Sources
Hardcopy , PDF
24-11-2020
English
26-10-2015
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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
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.
| DocumentType |
Standard
|
| Pages |
85
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
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.
| SAE AIR560C | Missile Hydraulic Pumps |
| SAE AIR4151 | Introduction to Starting Systems |
| SAE ARP699E | High Temperature Pneumatic Duct Systems for Aircraft |
| CFR 49(PTS400-571) : OCT 2017 | TRANSPORTATION |
| SAE J1775_201505 | 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 AIR1168/1 | 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 AIR1343B | 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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.