SYSTEM RELIABILITY PREDICTION BY FUNCTION. VOLUME II - PREDICTION PROCEDURE.
Abstract
A step-by-step procedure for predicting the reliability of Air Force Ground electronic sys tems during the pre-design stage is presented. Methods are outlined for predicting both a point value of the system mean time between failures, and a 95% confidence interval around this value. The reliability equations associated with the procedure appear in four forms; the form to utilize depends on the type of information avail able. Inputs to the prediction equations are data on certain system parameters, as defined herein. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1963
- Accession Number
- AD0418192
Entities
Organizations
- ARINC