Advanced Aircraft Electrical System (AAES). Definition and Prototype Design for F-14 Aircraft (GPMS)
Abstract
This report covering the amendment P00002 of contract N62269-75-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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1977
- Accession Number
- ADA047858
Entities
People
- P. Pisani
Organizations
- Grumman