This report covering the amendment P00002 of contract N-62269-75-C-0392 identifies a typical F-14A avionics suite for application and demonstration of the GPMS concept. This phase of the study concentrated on the multiplexing of avionics signals as opposed to the previous phase which described power generation and distribution approaches. A four terminal area multiplex scheme was selected to demonstrate multiplexing on an F-14A test aircraft. The compliment of power generation, power distribution and avionics multiplex equipment was revised to reflect the addition of GPMS and the installation in F-14A test aircraft No. 5. The requirements of each of the GPMS data terminals and their interfaces were identified. The design of data bus interface cards for future avionics encorporating MIL-STD-1553-A capability were developed and the volumes in a typical compliment of avionics were identified. (Author)
Advanced Aircraft Electrical System (AAES). Definition and Prototype Design for F-14 Aircraft (GPMS)
1977
181 pages
Report
No indication
English
Aircraft , Electrical equipment , Aircraft equipment , Jet fighters , Electric power distribution , Multiplexing , Avionics , Data transmission systems , Bus conductors , Logic circuits , Solid state electronics , Control systems , Flow charting , Specifications , Military requirements , F-14A aircraft , F-14 aircraft
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