HTPB-based Binder Surrogates and their Effects on Preliminary Rocket Motor Analyses
Adam Okniński
Słowa Kluczowe: hydroxyl-terminated polybutadiene, solid propellant, solid rocket motor, binder
DOI: 10.22211/cejem/154720
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HTPB-based Binder Surrogates and their Effects on Preliminary Rocket Motor Analyses
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