Current launch vehicle design emphasis is on low life-cycle cost. This paper applies total quality management (TQM) principles to a conventional systems design analysis process to provide low-cost, high-reliability designs. Suggested TQM techniques include Steward's systems information flow matrix method, quality leverage principle, quality through robustness and function deployment, Pareto's principle, Pugh's selection and enhancement criteria, and other design process procedures. TQM quality performance at least-cost can be realized through competent concurrent engineering teams and brilliance of their technical leadership.
Launch vehicle systems design analysis
AIAA, AHS, and ASEE, Aerospace Design Conference ; 1993 ; Irvine, CA, United States
1993-02-01
Conference paper
No indication
English
Launch Vehicle Systems Design Analysis
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