Theoretical analysis of the use of glycidyl polyazide and polynitratomethylmethyloxetane in high-performance reduced-smoke rocket propellants
Tomasz Gołofit, Katarzyna Cieślak, Michał Chmielarek
Keywords: solid rocket propellants, specific impulse, combustion temperature, HTPB, GAP, polyNIMMO, ammonium dinitramide, ammonium perchlorate
DOI: 10.22211/matwys/0237
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