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Design and Development of Hydrogen Peroxide Monopropellant Thruster: Basic Theory and Performance Calculations - Brossura
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Roughly in 1990’s, the concern about lower cost, more environmental friendly and non-toxic propellants showed that hydrogen peroxide can become as an alternative propellant to hydrazine and nitrogen tetroxide for those applications where these propellants were unacceptable. From this issues, the theory and performance calculation of hydrogen peroxide monopropellant thruster are theory concerning about the thrust produced by the thruster and designing of the thruster based on the require thrust. Design and Development of the thruster must be verify by the thruster performance from LabVIEW to the manual calculation. The performance will be compared between the model design and the experiment. Still, the theory and performance calculations falls short of being a complete theory of fundamental monopropellant thruster. Here, experiment results were shown,due to the effect during experiment,repeated experiment were done. From this issue, list of the method for preparing the thruster before firing must be followed by the proper steps and precautions were explained.
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Informazioni sull'autore
Mrs. Norazila Othman is a tutor at Universiti Teknologi Malaysia (UTM) with M.Eng. degree specializing in monopropellant rocket motor. Prof Dr. Subramaniam Krishnan and Prof Ir. Dr. Wan Khairuddin Wan Ali are from Faculty of Eng. and Technology, SRM University, India and Dept. of Aeronautics, Faculty of Mech. Eng., UTM, Malaysia respectively.
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Design and Development of Hydrogen Peroxide Monopropellant Thruster
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LAP Lambert Academic Publishing 2011-12, 2011
ISBN 10: 3846594067
ISBN 13: 9783846594063
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Design and Development of Hydrogen Peroxide Monopropellant Thruster
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Design and Development of Hydrogen Peroxide Monopropellant Thruster
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Design and Development of Hydrogen Peroxide Monopropellant Thruster Basic Theory and Performance Calculations
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Design and Development of Hydrogen Peroxide Monopropellant Thruster: Basic Theory and Performance Calculations
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LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846594067
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Design and Development of Hydrogen Peroxide Monopropellant Thruster: Basic Theory and Performance Calculations
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LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846594067
ISBN 13: 9783846594063
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Design and Development of Hydrogen Peroxide Monopropellant Thruster
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LAP LAMBERT Academic Publishing Dez 2011, 2011
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Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Roughly in 1990 s, the concern about lower cost, more environmental friendly and non-toxic propellants showed that hydrogen peroxide can become as an alternative propellant to hydrazine and nitrogen tetroxide for those applications where these propellants were unacceptable. From this issues, the theory and performance calculation of hydrogen peroxide monopropellant thruster are theory concerning about the thrust produced by the thruster and designing of the thruster based on the require thrust. Design and Development of the thruster must be verify by the thruster performance from LabVIEW to the manual calculation. The performance will be compared between the model design and the experiment. Still, the theory and performance calculations falls short of being a complete theory of fundamental monopropellant thruster. Here, experiment results were shown,due to the effect during experiment,repeated experiment were done. From this issue, list of the method for preparing the thruster before firing must be followed by the proper steps and precautions were explained. 192 pp. Englisch. Codice articolo 9783846594063
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Design and Development of Hydrogen Peroxide Monopropellant Thruster
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LAP LAMBERT Academic Publishing, 2011
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ISBN 13: 9783846594063
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Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Othman NorazilaMrs. Norazila Othman is a tutor at Universiti Teknologi Malaysia (UTM) with M.Eng. degree specializing in monopropellant rocket motor. Prof Dr. Subramaniam Krishnan and Prof Ir. Dr. Wan Khairuddin Wan Ali are from Facu. Codice articolo 5501960
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Design and Development of Hydrogen Peroxide Monopropellant Thruster : Basic Theory and Performance Calculations
Editore:
LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846594067
ISBN 13: 9783846594063
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Da: AHA-BUCH GmbH, Einbeck, Germania
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Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Roughly in 1990 s, the concern about lower cost, more environmental friendly and non-toxic propellants showed that hydrogen peroxide can become as an alternative propellant to hydrazine and nitrogen tetroxide for those applications where these propellants were unacceptable. From this issues, the theory and performance calculation of hydrogen peroxide monopropellant thruster are theory concerning about the thrust produced by the thruster and designing of the thruster based on the require thrust. Design and Development of the thruster must be verify by the thruster performance from LabVIEW to the manual calculation. The performance will be compared between the model design and the experiment. Still, the theory and performance calculations falls short of being a complete theory of fundamental monopropellant thruster. Here, experiment results were shown,due to the effect during experiment,repeated experiment were done. From this issue, list of the method for preparing the thruster before firing must be followed by the proper steps and precautions were explained. Codice articolo 9783846594063
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Design and Development of Hydrogen Peroxide Monopropellant Thruster
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Editorial Academica Espanola, 2011
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ISBN 13: 9783846594063
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Condizione: New. pp. 192. Codice articolo 2698162572
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