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The Study of Burning Characteristics of AP/HTPB/AL Basic Components of A Composite Propellant
Abstract
Department of Aeronautical Engineering, Universiti Teknologi Malaysia, 81310 UTM Skudai, Johor,
Malaysia
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PDFDOI: https://doi.org/10.37591/.v1i1-3.730
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eISSN: 2231-038X