DocumentCode :
2591266
Title :
Case study: application of contemporary reliability tools to the development of retrofit electronics
Author :
Duncan, Dennis L.
Author_Institution :
Alliant Techsyst. Inc., Everett, WA, USA
fYear :
1991
fDate :
29-31 Jan 1991
Firstpage :
525
Lastpage :
530
Abstract :
A case study of the successful application of reliability and maintainability principles is presented. Most of the current techniques for design evaluation, part selection, environmental stress screening, and reliability testing were applied in a cost-effective manner. Relative costs and pay back are compared for the different reliability-enhancing techniques. A high-reliability functional item replacement for the Torpedo Mark 48 ADCAP was developed. This device is known as the warhead electronics system (WES). The WES had to perform all of the existing function of the older designs it replaces, fit in the same form factor, and provide identical performance to the two devices it would replace. The WES had to be more readily repaired, supportable for the next 20 years, and easily enhanced with future performance improvements. Since this device is warhead related, it had to perform these functions with very high reliability. These objectives were all satisfactorily achieved despite a very restrictive schedule and funding constraints
Keywords :
electronic warfare; maintenance engineering; military equipment; reliability; Torpedo Mark 48 ADCAP; design evaluation; environmental stress screening; form factor; maintainability; part selection; reliability; retrofit electronics; warhead electronics system; Assembly; Computer aided software engineering; Costs; Design engineering; Finite impulse response filter; Guidelines; Job shop scheduling; Maintenance; Reliability engineering; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability and Maintainability Symposium, 1991. Proceedings., Annual
Conference_Location :
Orlando, FL
Print_ISBN :
0-87942-661-6
Type :
conf
DOI :
10.1109/ARMS.1991.154492
Filename :
154492
Link To Document :
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