Study of the Effect of Nitrated Hydroxyl-terminated Polybutadiene (NHTPB) on the Properties of Heterogeneous Rocket Propellants
Bogdan FLORCZAK, Rafał BOGUSZ, Wincenty SKUPIŃSKI, Michał CHMIELAREK, Arkadiusz DZIK
Słowa Kluczowe: NHTPB, HTPB, heterogeneous solid rocket propellant, linear burning rate
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