Azim Azmi. (2010). The influences of burning rate & mixing ratio of solid rocket propellant to produce constant thrust. Fakulti Kejuruteraan, UPNM Universiti Teknologi Malaysia.
Chicago Style (17th ed.) CitationAzim Azmi. The Influences of Burning Rate & Mixing Ratio of Solid Rocket Propellant to Produce Constant Thrust. Kuala Lumpur: Fakulti Kejuruteraan, UPNM Universiti Teknologi Malaysia, 2010.
MLA (9th ed.) CitationAzim Azmi. The Influences of Burning Rate & Mixing Ratio of Solid Rocket Propellant to Produce Constant Thrust. Fakulti Kejuruteraan, UPNM Universiti Teknologi Malaysia, 2010.
Warning: These citations may not always be 100% accurate.