Title:
A methodology for modeling the verification, validation, and testing process for launch vehicles
A methodology for modeling the verification, validation, and testing process for launch vehicles
| dc.contributor.advisor | Mavris, Dimitri N. | |
| dc.contributor.author | Sudol, Alicia | |
| dc.contributor.committeeMember | Schrage, Daniel | |
| dc.contributor.committeeMember | Pinon, Olivia | |
| dc.contributor.committeeMember | Kennedy, Graeme | |
| dc.contributor.committeeMember | Alexander, Reginald | |
| dc.contributor.department | Aerospace Engineering | |
| dc.date.accessioned | 2016-01-07T17:38:19Z | |
| dc.date.available | 2016-01-07T17:38:19Z | |
| dc.date.created | 2015-12 | |
| dc.date.issued | 2015-11-16 | |
| dc.date.submitted | December 2015 | |
| dc.date.updated | 2016-01-07T17:38:19Z | |
| dc.description.abstract | Completing the development process and getting to first flight has become a difficult hurdle for launch vehicles. Program cancellations in the last 30 years were largely due to cost overruns and schedule slips during the design, development, testing and evaluation (DDT&E) process. Unplanned rework cycles that occur during verification, validation, and testing (VVT) phases of development contribute significantly to these overruns, accounting for up to 75% of development cost. Current industry standard VVT planning is largely subjective with no method for evaluating the impact of rework. The goal of this research is to formulate and implement a method that will quantitatively capture the impact of unplanned rework by assessing the reliability, cost, schedule, and risk of VVT activities. First, the fidelity level of each test is defined and the probability of rework between activities is modeled using a dependency structure matrix. Then, a discrete event simulation projects the occurrence of rework cycles and evaluates the impact on reliability, cost, and schedule for a set of VVT activities. Finally, a quadratic risk impact function is used to calculate the risk level of the VVT strategy based on the resulting output distributions. This method is applied to alternative VVT strategies for the Space Shuttle Main Engine to demonstrate how the impact of rework can be mitigated, using the actual test history as a baseline. Results indicate rework cost to be the primary driver in overall project risk, and yield interesting observations regarding the trade-off between the upfront cost of testing and the associated cost of rework. Ultimately, this final application problem demonstrates the merits of this methodology in evaluating VVT strategies and providing a risk-informed decision making framework for the verification, validation, and testing process of launch vehicle systems. | |
| dc.description.degree | Ph.D. | |
| dc.format.mimetype | application/pdf | |
| dc.identifier.uri | http://hdl.handle.net/1853/54429 | |
| dc.language.iso | en_US | |
| dc.publisher | Georgia Institute of Technology | |
| dc.subject | Verification | |
| dc.subject | Validation | |
| dc.subject | Testing | |
| dc.title | A methodology for modeling the verification, validation, and testing process for launch vehicles | |
| dc.type | Text | |
| dc.type.genre | Dissertation | |
| dspace.entity.type | Publication | |
| local.contributor.advisor | Mavris, Dimitri N. | |
| local.contributor.author | Sudol, Alicia | |
| local.contributor.corporatename | Daniel Guggenheim School of Aerospace Engineering | |
| local.contributor.corporatename | Aerospace Systems Design Laboratory (ASDL) | |
| local.contributor.corporatename | College of Engineering | |
| local.relation.ispartofseries | Doctor of Philosophy with a Major in Aerospace Engineering | |
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| thesis.degree.level | Doctoral |