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Design and Development of the Lockheed C-5a Environmental Control System
Document Number: 680722
Date Published: February 1968
Author(s):
R. C. Bready - Lockheed-Georgia Co.
Abstract:
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.
Product Status: In Stock
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