Marshall Technical Reports Server

Comprehensive Design Reliability Activities for Aerospace Propulsion Systems

NASA/TP-209902, Christenson, R.L. and Whitley, M.R. and Knight*, K.C., Comprehensive Design Reliability Activities for Aerospace Propulsion Systems, Advanced Concepts Department, Space Transportation Directorate, NASA Marshall Space Flight Center, AL 35812, and*Sverdrup Technology, Huntsville, Alabama, January 2000, pp. 144, Format(s): PDF 5280k

View PDF
- Requires Adobe Acrobat Reader or other PDF viewer.

This technical publication describes the methodology, model, software tool, input data, and analysis results that support aerospace design reliability studies. The focus of these activities is on propulsion systems mechanical design reliability. The goal of these activities is to support design from a reliability perspective. Paralleling performance analyses in schedule and method, this requires the proper use of metrics in a validated reliability model useful for design, sensitivity, and trade studies. Design reliability analysis in this view is one of several critical design functions. A design reliability method is detailed and two example analyses are provided - one qualitative and the other quantitative. The use of aerospace and commercial data sources for quantification is discussed and sources listed. A tool that was developed to support both types of analyses is presented. Finally, special topics discussed include the development of design criteria, issues of reliability quantification, quality control, and reliability verification
Keywords:reliability, propulsion systems, mechanical systems, mechanical reliability, reliability analysis, design criteria, reliability verification, feas-m, quality control, design reliability, ucr, mps, failure rate
Subjects:Astronautics: Launch Vehicles And Launch Operations: Launch Vehicles
ID Code:508
Deposited On:24 July 2002