The influences of burning rate & mixing ratio of solid rocket propellant to produce constant thrust

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Bibliographic Details
Main Author: Azim Azmi
Corporate Authors: Universiti Pertahanan Nasional Malaysia Fakulti Kejuruteraan, Universiti Teknologi Malaysia Fakulti Kejuruteraan
Format: Thesis Book
Language:English
Published: Kuala Lumpur Fakulti Kejuruteraan, UPNM Universiti Teknologi Malaysia 2010
Series:Projek Sarjana Muda
Final Year Project
Undergraduate Project
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