Failure mode and effect analysis on safety critical components of space travel
| Autor: | Joseph Pineau, Kouroush Jenab |
|---|---|
| Rok vydání: | 2015 |
| Předmět: |
Space flight
Computer science business.industry lcsh:HF5735-5746 Criticality Analysis Real-time computing Process improvement ComputerApplications_COMPUTERSINOTHERSYSTEMS lcsh:Business records management Space (commercial competition) General Business Management and Accounting Failure mode effects and criticality analysis Solid Rocket Booster Criticality Risk analysis (engineering) Order (business) Business intelligence Critical design business Failure mode and effects analysis Failure Mode FMEA FMECA |
| Zdroj: | Management Science Letters, Vol 5, Iss 7, Pp 669-678 (2015) |
| ISSN: | 1923-9343 1923-9335 |
| DOI: | 10.5267/j.msl.2015.5.006 |
| Popis: | Article history: Received March 25, 2015 Received in revised format 28 March 2015 Accepted 12 May 2015 Available online May 14 2015 Sending men to space has never been an ordinary activity, it requires years of planning and preparation in order to have a chance of success. The payoffs of reliable and repeatable space flight are many, including both Commercial and Military opportunities. In order for reliable and repeatable space flight to become a reality, catastrophic failures need to be detected and mitigated before they occur. It can be shown that small pieces of a design which seem ordinary can create devastating impacts if not designed and tested properly. This paper will address the use of a Failure Mode, Effects, and Criticality Analysis (FMECA) with modified Risk Priority Number (RPN) and its application to safety critical design components of shuttle liftoff. An example will be presented here which specifically focuses on the Solid Rocket Boosters (SRBs) to illustrate the FMECA approach to reliable space travel. Growing Science Ltd. All rights reserved. 5 © 201 |
| Databáze: | OpenAIRE |
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