[PDF.86dz] 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
Norazila Othman, Subramaniam Krishnan, Wan Khairuddin Wan Ali
[PDF.vb93] Design and Development of Hydrogen Peroxide Monopropellant Thruster: Basic Theory and Performance Calculations
Design and Development of Norazila Othman, Subramaniam Krishnan, Wan Khairuddin Wan Ali epub Design and Development of Norazila Othman, Subramaniam Krishnan, Wan Khairuddin Wan Ali pdf download Design and Development of Norazila Othman, Subramaniam Krishnan, Wan Khairuddin Wan Ali pdf file Design and Development of Norazila Othman, Subramaniam Krishnan, Wan Khairuddin Wan Ali audiobook Design and Development of Norazila Othman, Subramaniam Krishnan, Wan Khairuddin Wan Ali book review Design and Development of Norazila Othman, Subramaniam Krishnan, Wan Khairuddin Wan Ali summary
| #8211967 in Books | 2011-12-29 | Original language:English | PDF # 1 | 8.66 x.44 x5.91l,.64 | File type: PDF | 192 pages||About the Author|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,
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 thruste...
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