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Aerospace Auxiliary Power Sources
- Aerospace Standard
- AIR744C
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
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.
Rationale
AIR744C has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
Unnamed Dataset 4 | ||
Unnamed Dataset 5 | ||
TABLE 1 | TYPICAL SOLID PROPELLANTS FOR GAS GENERATORS | |
TABLE 1 | TYPICAL SOLID PROPELLANTS FOR GAS GENERATORS | |
TABLE 2 | MONOPROPELLANT CHARACTERISTICS | |
TABLE 3A | ||
TABLE 3B | ||
TABLE 4 | ADVANTAGES AND DISADVANTAGES OF BLEED AIR APPLICATION | |
TABLE 6 | TYPICAL DATA FOR AIRCRAFT ENGINE JT3D-3B | |
TABLE 7 | TURBINE POWER COEFFICIENTS | |
TABLE 8 | COMMON BATTERY TYPES | |
TABLE 9 | COMPARISON OF PRIMARY BATTERIES | |
TABLE 10 | COMPARISON OF SECONDARY BATTERIES | |
TABLE 11 | SUMMARY TABLE | |
TABLE 12 | TYPES OF FUEL CELLS | |
TABLE 13 | APU/AIRCRAFT INTERFACE CONSIDERATIONS | |
TABLE 14 | FLYWHEEL MATERIAL PROPERTIES | |
TABLE 15 | FLYWHEEL GEOMETRY FOR AN OPTIMIZED DISK |
Issuing Committee
A6C4 is responsible for the development of standards, processes, and practices related to Fluid Power Sources (Pumps, Motors, Accumulators), and the integration of these components for Commercial and Military air vehicles. The panel provides a forum for government engineers, prime contractors, and suppliers to exchange technical information, regulatory updates, recent technology developments, issues related to system development and in service operation and lessons learned.
Reference
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