Othman norazila (16 risultati)

Paperback. Condizione: New.

Condizione: New.

Paperback. Condizione: New.

Condizione: New. In English.

Condizione: New. pp. 192.

Taschenbuch. Condizione: Neu. Design and Development of Hydrogen Peroxide Monopropellant Thruster | Basic Theory and Performance Calculations | Norazila Othman (u. a.) | Taschenbuch | 192 S. | Englisch | 2011 | LAP LAMBERT Academic Publishing | EAN 9783846594063 | Verantwortliche Person für die EU: OmniScriptum GmbH & Co. KG, Bahnhofstr. 28, 66111 Saarbrücken, info[at]akademikerverlag[dot]de | Anbieter: preigu. …

Paperback. Condizione: New.

Paperback. Condizione: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.

PAP. Condizione: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.

PAP. Condizione: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.

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.…

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.…

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.…

Condizione: New. Print on Demand pp. 192 2:B&W 6 x 9 in or 229 x 152 mm Perfect Bound on Creme w/Gloss Lam.

Condizione: New. PRINT ON DEMAND pp. 192.

Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. 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.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 192 pp. Englisch.…