Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
Reliability Improvement of a Solid Rocket Motor in Early Design Phases
Date
2009-07-01
Author
Bozkaya, Kenan
Akkök, Metin
Esin, Alp
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
205
views
0
downloads
Cite This
Designing a reliable system is difficult and costly, due to the design process to be followed and test requirements. It is important to consider reliability in very early design phases, and it is essential to select a baseline design with attainable high reliability. Therefore, in early phases, it is required to predict reliability and evaluate possible improvements for the reliability of the design alternatives in a fast manner to make necessary design decisions. In this study, a solid rocket motor is considered as a case study, and it is aimed to determine important parameters that affect the solid rocket motor reliability, to assess ballistic performance and casing structural reliability, and to find a new design point to evaluate possible improvement range for its reliability. The variations in dimensions and material properties, which are obtained from the previous data, are considered as the sources of failures and the limit states for acceleration, and the total impulse and the maximum stress in the casing are approximated by the response surface method. Monte Carlo simulation is used with the response surface functions to assess the failure probability and distributions of the rocket motor performance parameters. By considering the effect of the input parameters and distribution functions of the performance parameters, a new design point is proposed to decrease the total probability of failure.
Subject Keywords
Structural reliability
,
Response-Surface
URI
https://hdl.handle.net/11511/32372
Journal
JOURNAL OF SPACECRAFT AND ROCKETS
DOI
https://doi.org/10.2514/1.39609
Collections
Graduate School of Natural and Applied Sciences, Article
Suggestions
OpenMETU
Core
Reliability Analysis of Tactical Unmanned Aerial Vehicle (UAV)
Sürücü, Barış; Alemdaroğlu, Hüseyin Nafiz (2017-09-20)
To be competitive in the market, it is very important to design cost effective and reliable products. For this purpose, it is necessary to consider reliability as an integral part of the design procedure. Therefore, reliability which is a design parameter that affects cost and safety of a system should be taken into consideration in early phases since it is very difficult to change design at the later phases. Due to these causes the importance of reliability in manufacturing fields, especially in aviat...
Reliability of COSMIC Functional Size Measurement Results: A Multiple Case Study on Industry Cases
Top, Ozden Ozcan; Demirörs, Onur; Ozkan, Baris (2009-08-29)
Accuracy of the functional size is critical in software project management, since functional size is the most prevalent input for effort and cost estimation models. Functional size measurement is performed based on standardized manuals; however, the accuracy of FSM results is still based on the knowledge and cautions of the measurers. In this study we performed a multiple case study to identify the reliability of COSMIC and to observe the frequently encountered errors during functional size measurement. Pro...
Reliability analysis of tactical unmanned aerial vehicle (UAV)
Koç, Yılmaz; Alemdaroğlu, Hüseyin Nafiz; Sürücü, Barış; Department of Aerospace Engineering (2017)
To design cost effective and reliable products are considered to be important to be competitive in the Aerospace Industry. Reliability is therefore, taken as an integral part of the design process. Reliability, which is a kind of design parameter that affects cost and system safety, shall be taken into account in early phases of design process due to difficulties facing during changes in design at the later phases. Reliability of Tactical UAVs can be evaluated by reliability testing but these tests are very...
Prediction of geotechnical properties of cohesive soils from in-situ test : an evaluation of a local database
Yaman, Gökhan; Erol, Orhan; Department of Civil Engineering (2007)
In any geotechnical design procedure, the fundemantal point to be initially clearified is the characterization of existing soil profile at a site. This requires a great deal of planning a suitable site investigation program including borings, sampling, laboratory and in situ testing etc. Laboratory and in-situ (field) tests are important tools leading to the estimation of soils properties in geotechnics. Beside laboratory tests, the measurement of engineering properties in situ is a continuously growing and...
A New Design Approach for Rapid Evaluation of Structural Modifications Using Neural Networks
Demirkan, O.; Olceroglu, E.; BAŞDOĞAN, FATMA İPEK; Özgüven, Hasan Nevzat (2013-02-01)
Design optimization of structural systems is often iterative, time consuming and is limited by the knowledge of the designer. For that reason, a rapid design optimization scheme is desirable to avoid such problems. This paper presents and integrates two design methodologies for efficient conceptual design of structural systems involving computationally intensive analysis. The first design methodology used in this paper is structural modification technique (SMT). The SMT utilizes the frequency response funct...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
K. Bozkaya, M. Akkök, and A. Esin, “Reliability Improvement of a Solid Rocket Motor in Early Design Phases,”
JOURNAL OF SPACECRAFT AND ROCKETS
, pp. 914–922, 2009, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/32372.