Studies of the Influence of Nano Iron(III) Oxide on Selected Properties of Solid Heterogeneous Propellants Based on HTPB
Rafał BOGUSZ, Paulina MAGNUSZEWSKA, Bogdan FLORCZAK, Andrzej MARANDA, Katarzyna DROŻDŻEWSKA
Słowa Kluczowe: combustion rate modifier, nano iron(III) oxide, solid heterogeneous rocket propellant, HTPB, LRM
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