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Design and Development of the Lockheed C-5A Environmental Control System
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1968 by SAE International in United States
Annotation ability available
The C-5A bleed air control, air conditioning, temperature control, and fuselage pressurization systems are described. Peculiar design problems of this mammoth cargo transport are discussed with respect to the effect on system configurations and equipment design. A brief review is also presented on the development test programs conducted by the subsystem contractor and the air vehicle manufacturer.