AAES Laboratory Simulator Requirements (A-7 Aircraft).
Final rept. 27 Sep 77-27 Dec 78,
VOUGHT CORP DALLAS TEX
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This program was conducted for establishing requirements and developing specific design data for a hot bench mockup simulator. The simulator system being developed is based on the Advanced Aircraft Electrical System AAES Prototype Design evolved by the Vought Corp. under contract N62269-75-C-0391. The simulator system will ultimately be used by NADC to provide a laboratory verification of the operation and performance of the AAES in an aircraft weapon system environment. The evolved simulation design is formulated around the TA-7C aircraft electrical and avionic systems and the general physicalinstallation constraints of the TA-7C forward and mid fuselage sections. The designs developed under this contract were limited to electrical-avionic system definition and design. Simulator structural, system installation and wire harness designs will be developed under a follow-on contract. The designs developed under this contract include the full application of the AAES technologies to the TA-7C electrical and avionic subsystem and systems. The AAES technologies include HVDC High Voltage DC power generation, SOSTEL Solid State Electric Logic power distribution and management, and AMUX Avionic Multiplexing.
- Attack and Fighter Aircraft
- Training Aircraft
- Test Facilities, Equipment and Methods
- Electricity and Magnetism