<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE ArticleSet PUBLIC "-//NLM//DTD PubMed 2.7//EN" "https://dtd.nlm.nih.gov/ncbi/pubmed/in/PubMed.dtd">
<ArticleSet>
		<Article>
		<Journal>
			<PublisherName>International Journal of Nano Dimension (Int. J. Nano Dimens.)</PublisherName>
			<JournalTitle>Ti-alloys: Potential nano-modifier for Rocket Propellants</JournalTitle>
			<Issn></Issn>
			<Volume>Volume 7 (2016)</Volume>
			<Issue>Issue 2, May 2016</Issue>
			<PubDate PubStatus="epublish">
                <Year>2024</Year>
                <Month>02</Month>
                <Day>28</Day>
			</PubDate>
		</Journal>
		<ArticleTitle>Ti-alloys: Potential nano-modifier for Rocket Propellants</ArticleTitle>
		<VernacularTitle></VernacularTitle>
		<FirstPage></FirstPage>
		<LastPage></LastPage>
		<ELocationID EIdType="doi">10.7508/ijnd.2016.02.009</ELocationID>
		<Language>EN</Language>
		<AuthorList>
            			<Author>
                				<FirstName>Pragnesh</FirstName>
				<LastName>N. Dave</LastName>
				<Affiliation>Department of Chemistry, KSKV kachchh university, Bhuj Gujarat INDIA</Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            			<Author>
                				<FirstName>Parvin</FirstName>
				<LastName>N. Ram</LastName>
				<Affiliation>Department of Chemistry, KSKV kachchh university, Bhuj Gujarat INDIA</Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            			<Author>
                				<FirstName>Shalini</FirstName>
				<LastName>Chaturvedi</LastName>
				<Affiliation>Department of Chemistry, KSKV kachchh university, Bhuj Gujarat INDIA</Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            		</AuthorList>
		<PublicationType>Journal Article</PublicationType>
		<History>
			<PubDate PubStatus="received">
				<Year>2024</Year>
				<Month>02</Month>
				<Day>28</Day>
			</PubDate>
		</History>
		<Abstract>Composite solid propellants were prepared with and without nano-alloys (Ti-Co, Ti-Ni, Ti-Zn), where nano-alloys used as catalyst. These nano-alloys are prepared by hydrazine reduction method. Catalytic properties of these nanomaterials were measured on Ammonium perchorate/hydroxyterminatedpolybutadiene propellant by thermogravimetery analysis and differential thermal analysis. Both experimental results show enhance in the thermal decomposition of propellants in presence of nano-alloys. In this differential thermal analysis method experiments had done in 3 heating rate â1=5, â2=10, â3=15 degree on minute. Independent to model free; calculation of activation energy of high temperature decomposition step was done by using following kissinger equation. Burning rate of propellants is also calculated.</Abstract>
		<ObjectList>
            			<Object Type="keyword">
				<Param Name="value">Burning rate</Param>
			</Object>
						<Object Type="keyword">
				<Param Name="value">Propellants</Param>
			</Object>
						<Object Type="keyword">
				<Param Name="value">Thermal decomposition</Param>
			</Object>
						<Object Type="keyword">
				<Param Name="value">Activation Energy</Param>
			</Object>
						<Object Type="keyword">
				<Param Name="value">Ammonium perchlorate</Param>
			</Object>
					</ObjectList>
	</Article>
	</ArticleSet>
