Search In this Thesis
   Search In this Thesis  
العنوان
An Experimental Study of Mechanical characteristics and Burning Rate of Different Types of Composite Solid Propellan :
المؤلف
NourEldin, Ahmed Fouad Ibrahim Khalid.
هيئة الاعداد
باحث / Ahmed Fouad Ibrahim Khalid NourEldin
مشرف / Mostafa Ahmed Ismail
مشرف / Youssef Ahmed Attai
مشرف / Youssef Ahmed Attai
الموضوع
Composite Solid Propellant.
تاريخ النشر
2022.
عدد الصفحات
I-XIII, 65 p. :
اللغة
الإنجليزية
الدرجة
ماجستير
التخصص
الهندسة الميكانيكية
تاريخ الإجازة
1/1/2022
مكان الإجازة
جامعة حلوان - كلية الهندسة - المطرية - هندسة القوى الميكانيكية
الفهرس
Only 14 pages are availabe for public view

from 79

from 79

Abstract

Research Objective
The main goal of this thesis is to investigate the changing in the tensile behavior (mechanical properties), and the burning rate characteristics (ballistic characteristics) of hydroxyl-terminated polybutadiene (HTPB) propellant under the variations of the crosslinking density, which was predominantly determined by the equivalent ratio of diisocyanate to total hydroxyl (NCO/OH ratio), which known as the curing ratio.
Objective
The main objective of this literature survey is to investigate the mechanical properties and ballistic characteristics with a change in curing ratios on solid propellant in order to detect the behavior of the solid propellant. And an investigation of the effect of temperature change on stress and elongation, the stress increases with increasing temperature and the elongation decreases with decreasing temperature. To study a change in curing ratios on the burning rate, it has a slight effect with increasing the burning rate.