Reliability Analysis of a Solid Rocket Motor Based on Response Surface Method and Monte Carlo Simulation

Bozkaya, Kenan; Sumer, B. Mutlu; Kuran, Bayindir; Ak, Metin

doi:10.2514/6.2005-3598

Cited by 9 publications

(2 citation statements)

References 5 publications

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“…The reliability of the composite configuration was also calculated. Bozkaya et al [18,19] and Akpan and Wong [20] developed some useful and efficient methods for the sensitivity analysis and reliability calculations [21] based on surface response methods (SRM) and Monte Carlo simulation techniques.…”

Section: Introductionmentioning

confidence: 99%

Probabilistic Reliability Analysis of Carbon/Carbon Composite Nozzle Cones with Uncertain Parameters

Xie¹,

Yang²,

Meng³

et al. 2019

Journal of Spacecraft and Rockets

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Section: Introductionmentioning

confidence: 99%

Probabilistic Reliability Analysis of Carbon/Carbon Composite Nozzle Cones with Uncertain Parameters

Xie¹,

Yang²,

Meng³

et al. 2019

Journal of Spacecraft and Rockets

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“…Kim et al (2014Kim et al ( , 2015 performed reliability analysis based on RSM to predict structural failure modes of a motor case in their studies. Bozkaya et al (2005) preferred usage of RSM and Monte Carlo simulation to perform reliability analysis of geometrical variations of a SRM. Vaidyanathan et al (2000) compared neural network and RSM examining different rocket engine components.…”

Section: Introductionmentioning

confidence: 99%

Solid rocket motor design using a surrogate model

Tola

Nikbay

2018

AEAT

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Purpose This study aims to determine the relationship between sectional geometric parameters of a slotted solid rocket propellant on structural integrity and internal ballistic performance of a rocket motor by using response surface method. Design/methodology/approach Zero-dimensional (0D) ballistic solver is developed and validated to determine the effects of sectional geometric parameters on internal ballistic performance of a rocket motor. Additionally, effects of these parameters on structural strength of the system are examined by performing linear viscoelastic finite element analysis under plane strain assumption. Results of the 0D internal ballistic analyses are used as an input to the structural analysis. Findings Different response surfaces are constructed to represent the characteristic variation of solid propellant’s structural strength and internal ballistic performance with respect to design variables. Originality/value Coupled analysis methodology in terms of structural strength and internal ballistic performance presented in this work facilitates many designers who are working on solid rocket motor development. This study represents graphical results summarizing effects of sectional parameters of a slotted grain on both internal ballistic performance and structural strength results. Additionally, graphical results summarizing the effects of sectional parameters on structural strength and internal ballistic performance provide useful information for researchers that lessens design period. Finally, validations presented in this work can also be used as a benchmark reference for different studies.

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Robust Regression Metamodelling of Complex Systems: The Case of Solid Rocket Motor Performance Metamodelling

Kartal-Koç

Batmaz

Weber

2012

Advances in Intelligent Modelling and Simulation

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Reliability Analysis of a Solid Rocket Motor Based on Response Surface Method and Monte Carlo Simulation

Cited by 9 publications

References 5 publications

Probabilistic Reliability Analysis of Carbon/Carbon Composite Nozzle Cones with Uncertain Parameters

Probabilistic Reliability Analysis of Carbon/Carbon Composite Nozzle Cones with Uncertain Parameters

Solid rocket motor design using a surrogate model

Robust Regression Metamodelling of Complex Systems: The Case of Solid Rocket Motor Performance Metamodelling

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