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		<title>Hybrid Rocket Fuel: PVC/DBP Combustion Efficiency Insights</title>
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		<pubDate>Mon, 19 Jan 2026 00:22:39 +0000</pubDate>
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		<category><![CDATA[Combustion Efficiency]]></category>
		<category><![CDATA[Hybrid propulsion systems]]></category>
		<category><![CDATA[Hybrid rocket fuel]]></category>
		<category><![CDATA[İşte 5 uygun etiket: **Hybrid rocket propulsion]]></category>
		<category><![CDATA[PVC/DBP combustion]]></category>
		<category><![CDATA[PVC/DBP fuel]]></category>
		<category><![CDATA[Regression rate]]></category>
		<category><![CDATA[Regression rate analysis]]></category>
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					<description><![CDATA[In the rapidly advancing field of aerospace engineering, hybrid rocket technologies are garnering significant attention, especially as researchers seek to optimize combustion efficiencies and thrust characteristics. A recent innovative study conducted by Pawar, Praveen, and Chavhan sheds light on the intricacies of combustion processes and the potential of utilizing polyvinyl chloride (PVC) combined with dibutyl [&#8230;]]]></description>
		
		
		
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