Aging investigation of composite solid propellant / Ahmed Mohammed Aboelmagd Salem ; Supervised Ehab Fouad Abadir , Sahar Mohammed Elmarsafy , Amgad Ahmed Aly

By:

Ahmed Mohammed Aboelmagd Salem

Contributor(s):

Material type: Text

TextLanguage: English Publication details: Cairo : Ahmed Mohammed Aboelmagd Salem , 2011Description: 82 P. : charts , facsimiles ; 30cmOther title:

استنتاج تقادم العمر الإفتراضى للوقود الصلب المختلط [Added title page title]

Subject(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 purpose of this research is to study the composit solid propellant and studying the effect of bonding agents , curative ratio and burning rate modifiers on the propellant mechanical charateristics by applying an accelerated aging program for 26 weeks at temperature ( 65 {u00B0}C ) and comparing these results with a standard aged sample to give a reliable aging program , which allows the prediction of the propellant service life time

Tags from this library: No tags from this library for this title. Log in to add tags.

Average rating: 0.0 (0 votes)

Holdings
Item type	Current library	Home library	Call number	Copy number	Status	Date due	Barcode
Thesis	قاعة الرسائل الجامعية - الدور الاول	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.04.M.Sc.2011.Ah.A (Browse shelf(Opens below))		Not for loan		01010110055842000
CD - Rom	مخـــزن الرســائل الجـــامعية - البدروم	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.04.M.Sc.2011.Ah.A (Browse shelf(Opens below))	55842.CD	Not for loan		01020110055842000

Browsing المكتبة المركزبة الجديدة - جامعة القاهرة shelves Close shelf browser (Hides shelf browser)

Previous	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	Next
Previous	Cai01.13.04.M.Sc.2010.Ta.U Using modified polyvinyl chloride in thermal insulation of solid propellant grain /	Cai01.13.04.M.Sc.2010.Ta.U Using modified polyvinyl chloride in thermal insulation of solid propellant grain /	Cai01.13.04.M.Sc.2011.Ah.A Aging investigation of composite solid propellant /	Cai01.13.04.M.Sc.2011.Ah.A Aging investigation of composite solid propellant /	Cai01.13.04.M.Sc.2011.Ah.C Comparative study between different fillers used as reinforcements of rubber thermal insulators /	Cai01.13.04.M.Sc.2011.Ah.C Comparative study between different fillers used as reinforcements of rubber thermal insulators /	Cai01.13.04.M.Sc.2011.Ah.M Microscopic modeling of the free board and fluidized bed inside the melter - gasifier of optimized corex ironmaking process /	Next

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

The purpose of this research is to study the composit solid propellant and studying the effect of bonding agents , curative ratio and burning rate modifiers on the propellant mechanical charateristics by applying an accelerated aging program for 26 weeks at temperature ( 65 {u00B0}C ) and comparing these results with a standard aged sample to give a reliable aging program , which allows the prediction of the propellant service life time

Issued also as CD

There are no comments on this title.

to post a comment.