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Modeling And Analysis Of Rocket Outer Shell
[Full Text]
AUTHOR(S)
Sheikh Naunehal Ahamed, Jadav Vijay Kumar, Mohammed Mushraffuddin, Parimi Sravani
KEYWORDS
Index Terms: Multistaging, Finite Element Method, Catia, Hypermesh, Ansys, Epoxy-carbon
ABSTRACT
Abstract: The research aims at modeling a rocket case to accomplish mission requirements. The various reasons that may cause case failures are improper design and analysis, lack of non-destructive tests during critical phases of fabrication, negligence in service conditions, improper material selection. Hence it’s very essential to model rocket with perfect designing and analysis. This journal entails the designing of rocket case using Catia V5, meshing with Hypermesh and Analysis with Ansys, where different materials like Aluminium and Epoxy-carbon are selected. The results focus on the deformation produced under same loading condition in two different materials and studying the results.
REFERENCES
[1]. NASA space vehicle design criteriahttp://ntrs.nasa.gov/archive
[2]. Aircraft Structures for Engineering Students by T.H.G. Meghson
[3]. Metal in rocket constructswww.tripoli.org
[4]. The rocket structural systemexploration.grc.nasa.gov/education
[5]. Multi-stage rockets, Valkyrie report no. 5105
[6]. Morton-thiokol’s “rocket basics”.
[7]. Rocket casingwww.fas.org
[8]. Structure and Properties Of Engineering Materials by V. S. R. Murthy
[9]. Introduction to flight, 5th edition by Anderson
[10]. Material propertieshttp://www-materials.eng.cam.ac.uk
[11]. Spacecraft Structures by J. Jaap Wijker
[12]. 12.Introduction to rocket science and engineering by Travis S. Taylor
[13]. Introduction To Ansys 10.0by R.B. Choudary
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