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
Subjects:
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Call Number :psm SZM .A590 2010

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245 1 4 |a The influences of burning rate & mixing ratio of solid rocket propellant to produce constant thrust  |c Azim Azmi 
260 |a Kuala Lumpur  |b Fakulti Kejuruteraan, UPNM  |b Universiti Teknologi Malaysia  |c 2010 
300 |a xv, 66 p.  |b ill.  |c 30 cm. 
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490 1 |a Final Year Project 
490 1 |a Undergraduate Project 
502 |a Projek Sarjana Muda  |b Sarjana Muda Kejuruteraan Mekanikal 
502 |a Final Year Project  |b Bachelor of Mechanical Engineering 
502 |a Undergraduate Project  |b Bachelor of Mechanical Engineering 
504 |a Includes bibliographical references 
592 |c Hadiah & sumbangan  |h UPNM/UTM 
655 |a Sarjana Muda Kejuruteraan Mekanikal 
655 |a Bachelor of Mechanical Engineering 
710 2 |a Universiti Pertahanan Nasional Malaysia  |b Fakulti Kejuruteraan 
710 2 |a Universiti Teknologi Malaysia  |b Fakulti Kejuruteraan 
830 0 |a Projek Sarjana Muda 
830 0 |a Final Year Project 
830 0 |a Undergraduate Project 
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