Some important base line requirements for commercial aircraft propulsion systems; in summary, engines must be designed to be installed in aircraft not on test stand; decision must be directed toward long life, ease of repair, and good long term installed performance; all power plant subsystems must be integrated into installation, tested early and throughly as part of power plant, and be more reliable and maintainable than current equipment in service. (15346)
Design requirements and objectives for commercial aircraft propulsion systems
ASME Paper
ASME Meeting GT-57 ; 1969 Design
1969
11 pages
Conference paper
English
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