Design and Development of the Lockheed C-5A Environmental Control System

680722

02/01/1968

Event
National Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/680722
Pages
16
Citation
Bready, R., "Design and Development of the Lockheed C-5A Environmental Control System," SAE Technical Paper 680722, 1968, https://doi.org/10.4271/680722.
Additional Details
Publisher
Published
Feb 1, 1968
Product Code
680722
Content Type
Technical Paper
Language
English