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study of combustion behaviour of the low oxygen content composite solid propellants / Wael Mohamed Ahmed Abdelwareth , supervised Mohamed Amin Elshahir Sadek , Shokry Abdelsamee Shokry , Ahmed Hussien Elahwany

By: Contributor(s): Language: Eng Publication details: Cairo : Wael Mohamed Ahmed Abdelwareth , 2006Description: 159 P. : ill. ; 30cmSubject(s): Available additional physical forms:
  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty Of Engineering - Department Of Chemical Engineering Summary: The composite low oxygen contentpropellants (LOCP) are typically used for ram rocket ducted rocket motors the low oxygen content propellants (LOCP) are characterized by their low combustion temperature and their specific impulse is low
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Item type Current library Home library Call number Copy number Status Date due Barcode
Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.04.M.Sc.2006.Wa.S. (Browse shelf(Opens below)) Not for loan 01010110045531000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.04.M.Sc.2006.Wa.S. (Browse shelf(Opens below)) 45531.CD Not for loan 01020110045531000

Thesis (M.Sc.) - Cairo University - Faculty Of Engineering - Department Of Chemical Engineering

The composite low oxygen contentpropellants (LOCP) are typically used for ram rocket ducted rocket motors the low oxygen content propellants (LOCP) are characterized by their low combustion temperature and their specific impulse is low

Issued also as CD

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