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
Article (PDF, 1.0 MB)
