Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/401873
Title: Investigation on the effect of thrust chamber geometric parameters on the performance of NTO_MMH thrusters
Researcher: Arun Kumar, P
Guide(s): Balachandran, P
Keywords: Cold Flow Evaluation
Effect of Contraction Ratio on Performance
Engineering
Engineering and Technology
Engineering Mechanical
Hypergolicity of Liquid Propellant
Influence of Thrust Chamber Geometry
Liquid Rocket Engine Modelling,
University: University of Kerala
Completed Date: 2015
Abstract: Abstract available newline newline
Pagination: i-viii, 167p.
URI: http://hdl.handle.net/10603/401873
Appears in Departments:Faculty of Engineering and Technology

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01_title.pdfAttached File51.62 kBAdobe PDFView/Open
02_declaration.pdf51.07 kBAdobe PDFView/Open
03_certificate.pdf52.38 kBAdobe PDFView/Open
04_acknowledgements.pdf64.33 kBAdobe PDFView/Open
05_abstract.pdf119.31 kBAdobe PDFView/Open
06_contents.pdf76.7 kBAdobe PDFView/Open
07_list of figures.pdf108.03 kBAdobe PDFView/Open
08_list of tables.pdf54.2 kBAdobe PDFView/Open
09_nomenclature or abbreviations.pdf81.3 kBAdobe PDFView/Open
10_chapter 1.pdf296.7 kBAdobe PDFView/Open
11_chapter 2.pdf184.29 kBAdobe PDFView/Open
12_chapter 3.pdf658.73 kBAdobe PDFView/Open
13_chapter 4.pdf568.62 kBAdobe PDFView/Open
14_chapter 5.pdf5.86 MBAdobe PDFView/Open
15_chapter 6.pdf202.79 kBAdobe PDFView/Open
16_publications arising out of the research work.pdf61.97 kBAdobe PDFView/Open
17_paper to be presented or published.pdf61.96 kBAdobe PDFView/Open
18_appendices.pdf1.49 MBAdobe PDFView/Open
19_references.pdf144.56 kBAdobe PDFView/Open
80_recommendation.pdf248.97 kBAdobe PDFView/Open
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