In this paper, the factors effecting the shock wave and impact Sensitivity such as oxygen balance, porosity, components particle size in composite solid propellants have been investigated. The energetic components of propellants such as oxidizer and fuel usually effect shock wave sensitivity and changing in composition, particle size and manufacturing process, determine the sensitivity property...

GAP propellants has good performance due to high energy of this polymer. Unfortunately, due to poor flexibility of GAP polymer and presence of rigid and conjugated azide side groups in its structure, they have poor mechanical properties especially under low temperatures. This article deals with methods of improving mechanical properties of solid composite propellants based on GAP through changi...

Abstract In this study, the effect of additives such as ammonium oxalate (AO), mixture of ammonium oxalate and strontium carbonate (SC) on AP/HTPB based composite propellants was investigated by burning rate, DTA, density and autoignition temperature measurements. The results show that the burning rates of these propellants are decreased significantly. DTA and autoignition temperature experime...

In this article the aging of HTPB based composite solid propellants have been studied by Van’t Hoff method. The F-factor of Van’t Hoff equation was calculated by dynamic mechanical analysis (DMA) for reference propellants sample that was equal 2.5. Then the accelerated aging program conditions have been determined by Van’t Hoff equation. According to accelerated aging program the reference prop...

In this article aging behavior of composite solid propellant was investigated by determining its mechanical properties at elevated temperatures. For this purpose, three HTPB samples with different microstructures were selected and composite solid propellants were prepared based on them keeping similar other components and aging was studied by accelerated method.  Mechanical properties were meas...

Iron oxide as a burning rate catalyst commonly used in many of solid composite propellants. As the particle size of this component decreased, the final properties of the propellant change. In this research, effects of using 1 percent by weight of nano hematite iron oxide (α-Fe2O3) investigated on properties of an HTPB/AP/Al formulation and compared with the same propellant containing micronized...

چکیده استخراج و اندازه گیری فنولیک اسیدهای وانیلیک، کافئیک، پاراکوماریک و فرولیک از عسل چندگیاه توسط استخراج فاز جامد (spe) با کارتریج c18 و روش کروماتوگرافی مایع با کارایی بالا (hplc) انجام شد. بهینه سازی شرایط spe و جداسازی با hplc، با استفاده از طرح مرکب مرکزی (ccd) انجام شد. به منظور دست یابی به حداکثر بازیابی فنولیک اسیدها از عسل، پنج فاکتور آزمایشی: ph محلول نمونه، حجم و ph مایع شستشو، ن...