Title of article
UJIAN PEMBAKARAN PROPELAN ROKET PEPEJAL
Author/Authors
Jaafar, Mohammad Nazri Mohd. Universiti Teknologi Malaysia - Fakulti Kejuruteraan Mekanikal - Jabatan Kejuruteraan Aeronautik, Malaysia , Wan Ali, Wan Khairuddin Universiti Teknologi Malaysia - Fakulti Kejuruteraan Mekanikal - Jabatan Kejuruteraan Aeronautik, Malaysia , Zahri, Ahmad Saufi Mohamed Universiti Teknologi Malaysia - Fakulti Kejuruteraan Mekanikal - Jabatan Kejuruteraan Aeronautik, Malaysia
From page
13
To page
28
Abstract
The composition of lacquer and fuel used during fabrication of solid propellant affects the burning rates. This study shows the effect of varying the percentage composition of both items. Results obtained show that the burning rates reduce with increase in laker percentage when fuel was set constant at 29%. However, when lacquer was set constant at 22% and at varied fuel compositions, the burning rates show a parabolic plot with the optimum composition at 28.6% fuel.
Keywords
Kalium nitrate , sulfur , aluminium , burning rate , solid rocket
Journal title
Jurnal Teknologi :F
Journal title
Jurnal Teknologi :F
Record number
2715558
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