Fault Tolerant Electrical Power System. Phase I. Study.
Abstract
This report documents the results of Phase I, Study, of this five phase program. The objectives of this program are to develop an FTEPS design for an ATF aircraft and to design and fabricate a low cost FTEPS demonstrator with an integrated load simulator. The primary purpose of the program is to develop an electrical power generation and distribution system that can supply electrical power to the various critical systems on the aircraft with a reliability and power quality level commensurate with the requirements of the loads. In Phase I, the electrical loads and their power requirements were defined for the ATF baseline aircraft model. The loads were also located in the baseline aircraft model.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1986
- Accession Number
- ADA177061
Entities
People
- David L. Sommer
- Mark W. Dige
- Patrick J. Leong
Organizations
- Boeing Military Aircraft