| 000 | 01685cam a2200337 a 4500 | ||
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| 003 | EG-GiCUC | ||
| 005 | 20250223030241.0 | ||
| 008 | 100714s2010 ua d f m 000 0 eng d | ||
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_aEG-GiCUC _beng _cEG-GiCUC |
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| 041 | 0 | _aeng | |
| 049 | _aDeposite | ||
| 097 | _aM.Sc | ||
| 099 | _aCai01.12.08.M.Sc.2010.Fa.A | ||
| 100 | 0 | _aFarag Sobh Farag Mohamed Helal | |
| 245 | 1 | 0 |
_aAnalytical studies and performance characteristics for some solid propellants / _cFarag Sobh Farag Mohamed Helal ; Supervised N. T. Abdelghani , Said Elmeniawy |
| 246 | 1 | 5 | _aدراسات تحليلية و خواص الأداء لبعض المواد الدافعة الصلبة |
| 260 |
_aCairo : _bFarag Sobh Farag Mohamed Helal , _c2010 |
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| 300 |
_a134 Leaves : _bcharts ; _c30cm |
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| 502 | _aThesis (M.Sc.) - Cairo University - Faculty of Science - Department of Analytical Chemistry | ||
| 520 | _aThe influence of different burning rate modifiers (catalysts) on the double base rocket propellants was studies. HPLC, GC and AAS were used to investigate and check the components of the propellant samples. Able heat test, bergman and junk test, methyl violet test, lenze and pleuss test, explosion temperature and calorimetric value were used to study the effect of these modifiers on thermal stability of these propellants | ||
| 530 | _aIssued also as CD | ||
| 653 | 4 | _aBurning rate modifiers | |
| 653 | 4 | _aDouble base propellants | |
| 653 | 4 | _aPropellants | |
| 700 | 0 |
_aN. T. Abdelghani , _eSupervisor |
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| 700 | 0 |
_aSaid Elmeniawy , _eSupervisor |
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| 856 | _uhttp://172.23.153.220/th.pdf | ||
| 905 |
_aMustafa _eRevisor |
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| 905 |
_aSamia _eCataloger |
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| 942 |
_2ddc _cTH |
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_c30789 _d30789 |
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