Application of scenario-driven hazard analysis in the solid rocket booster

  • Authors

    • Kouroush Jenab Embry-Riddle Aeronautical University
    • Nikita Ottosen Embry-Riddle Aeronautical University
    • Saeid Moslehpour Hartford University
    2016-01-07
    https://doi.org/10.14419/ijet.v5i1.4673
  • Solid Rocket Booster, Field Joint, Scenario-Driven Hazard Analysis.
  • Abstract

    Bibliographical Notes: Kouroush Jenab is a senior member of IEEE, received the B.Sc. degree from the IE Department at Isfahan University of Technology (1989), the M.Sc. degree from the IE Department at Tehran Polytechnic (1992), and the Ph.D. degree from the Department of Mechanical Engineering at the University of Ottawa (2005). He served as a senior engineer/manager in auto, and high-tech industries for 18 years. He joined the National Research Council Canada as a research officer where he participated in several international research projects. In 2006, he joined the Department of Mechanical and Industrial Engineering at Ryerson University, Toronto as assistant professor. Currently, Dr. Jenab is Faculty of the College of Aeronautics at Embry-riddle Aeronautical University, FL, USA. He has published over 110 papers in international scientific journals based on his experiences in industries.

    Nikita Ottosen is a current Systems Engineering graduate student at Embry-Riddle Aeronautical University. She received her undergraduate degree from ERAU in Aeronautics and is currently working as an Assistant Campus Director at the Crestview, FL campus. She gained valuable knowledge previously working for the Boeing Company and Seattle-Tacoma International Airport, known as The Port of Seattle, in Seattle, Washington. During her time at The Port of Seattle she worked alongside the Wildlife Management department to conduct a study on effective wildlife management strategies. Her study will become a part of a future Airport Cooperative Research Program (ACRP) publication, sponsored by the FAA’s Transportation Research Board of the National Academies.

    Saeid Moslehpour is a full professor and department chair in the Electrical and Computer Engineering Department in the College of Engineering, Technology, and Architecture at the University of Hartford. He holds Ph.D. (1993) from Iowa State University and Bachelor of Science (1989) and Master of Science (1990) degrees from University of Central Missouri. His research interests include failure analysis, logic design, CPLDs, FPGAs, Embedded electronic system testing and distance learning.

  • References

    1. [1] Bos, Carole "Solid Rocket Booster - Exploded View" AwesomeStories.com. Retrieved from http://www.awesomestories.com/asset/view/Solid-Rocket-Booster-Exploded-View on March 3, 2015.

      [2] Dismukes, K. (2002, October 22). Space Shuttle Basics. Retrieved from National Aeronautics and Space Administration: Retrived from http://spaceflight.nasa.gov/shuttle/reference/basics/srb/index.html on March 3, 2015.

      [3] Dumoulin, J. (2015, February 25). NSTS 1988 Shuttle Reference Manual. Retrieved from National Aeronautics and Space Administration: Retrived from http://science.ksc.nasa.gov/shuttle/technology/sts-newsref/srb.html#srb on March 3, 2015.

      [4] Environmental Protection Agency. (2012, July 31). Risk Assessment. Retrieved from United States Environmrntal Protection Agency: Retrived from http://epa.gov/riskassessment/basicinformation.htm#arisk on March 5, 2015.

      [5] Harris, A. (2013, October 31). 6 Unexpected Ways Six Sigma Can Benefit Your Company. Retrieved from Process Excellence Network: http://www.processexcellencenetwork.com/lean-six-sigma-business-transformation/articles/6-ways-six-sigma-can-benefit-your-company/ on March 2, 2015.

      [6] Hammer, W. (1972). Handbook of System and Product Safety. Englewood Cliffs, NJ: Prentice-Hall.

      [7] Hoover, K., & Fowler, W. (23, February 2015). Spacecraft design archive. Retrieved from Texas Space Grant Consortium: Retrived from http://www.tsgc.utexas.edu/archive/general/ethics/boosters.html on MArch 3, 2015.

      [8] Ionita, M. T., America, P., Hammer, D. K., Obbink, H., & Trienekens, J. J. (2004). A Scenario-Driven Approach for Value, Risk, and Cost Analysis in System Architecting for Innovation. In Software Architecture (pp. 277, 280). The Netherlands. http://dx.doi.org/10.1109/wicsa.2004.1310709.

      [9] Jenab, K. (2015, March 15). Technical Risk Management. Daytona Beach, Florida, United States.

      [10] Jenab K. & Nicol T. (In Press). The Use of Perturbation with Monte Carlo Simulation Approach to Estimating the Reliability of the Space Shuttle Field Joints. International Journal for Computational Methods in Engineering Science & Mechanics.

      [11] Jenab K., Herrin J., & Khoury S. (2015). System hazard platform: Case study NASA field joint failure. International Journal Mechanical Engineering Research, 5(2), 9-16. http://dx.doi.org/10.5539/mer.v5n2p9.

      [12] Jenab K., Blecher R.M., & Moslehpour S. (In Press). SRB field joints failure analysis using fuzzy FMEA. International Journal of Physics and Astronomy. 3(1), 1-20. http://dx.doi.org/10.15640/ijpa.v3n1a1.

      [13] Jenab K. & Moslehpour S. (2015). Failure analysis: Case study challenger SRB field joint. International Journal of Engineering and Technology. 8(6), In Press.

      [14] Jenab K., Fine T., Khoury S., & Moslehpour S. (2015). Cause-Consequence analysis for NASA’s space transportation system (STS) - solid rocket booster (SRB). International Journal of Business and Management. 10(8), 23-28. http://dx.doi.org/10.5539/ijbm.v10n8p23.

      [15] Jenab K., Khoury S., & Rodriguez S. (2015). Effective FMEA analysis or not? Strategic Management Quarterly. 3(2), 25-36. http://dx.doi.org/10.15640/smq.v3n2a2.

      [16] Jenab K. & Kelley T. K. (2015). Bayesian Failure Modes and Effects Analysis: Case Study for the 1986 Challenger Failure. International Journal of Engineering Research and Technology. 4(5), 685-690.

      [17] Jenab K. & Pineau J. (2015). Failure Mode and Effect Analysis on Safety Critical Components of Space Travel. Management Science Letters. 5(7), 669-678. http://dx.doi.org/10.5267/j.msl.2015.5.006.

      [18] John F. Kennedy Space Center. (1994, September). Space Shuttle Solid Rocket Booster Retrieval Ships. Retrieved from NASA Facts Online: http://www-pao.ksc.nasa.gov/kscpao/nasafact/ships.htm.

      [19] Leone, D. (2011, June 18). NASA's New Heavy-Lift Launcher Would First Fly With Solid Rocket Booster. Retrieved from Space.com: http://www.space.com/12006-nasa-heavy-lift-rocket-design-includes-solid-boosters.html.

      [20] Main, B. W. (2004). Risk assessment. Professional Safety, 49(12), 37-47. Retrieved from <http://search.proquest.com.ezproxy.libproxy.db.erau.edu/docview/200367853?accountid=27203> on March 3, 2015.

      [21] NASA. (1986, June 6). The Presidential Commison on the Sapce Shuttle Challenger Accident Report. Retrieved from National Aeronautics and Space Administration: http://science.ksc.nasa.gov/shuttle/missions/51-l/docs/rogers-commission/Chapter-4.txt on March 3, 2015.

      [22] Szondy, D. (2012, October 4). NASA building world's largest solid-fuel rocket. Retrieved from Gizmag: http://www.gizmag.com/sls-largest-solid-rocket/24408/ on March 3, 2015.

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  • How to Cite

    Jenab, K., Ottosen, N., & Moslehpour, S. (2016). Application of scenario-driven hazard analysis in the solid rocket booster. International Journal of Engineering & Technology, 5(1), 16-19. https://doi.org/10.14419/ijet.v5i1.4673