AAES Laboratory Simulator Requirements (A-7 Aircraft).
Abstract
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 physical/installation 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).
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1978
- Accession Number
- ADA066393
Entities
People
- A. J. Marek
- D. E. Lautner
- J. R. Perkins
- Jacob L. Jones
Organizations
- Vought