Studies on the Effect of Nano-MnO2 in HTPB-based Composite Propellant Formulations
Dhirendra R. Kshirsagar, Sunil Jain, Sumit Bhandarkar, Manoj Vemuri, Mehilal
Słowa Kluczowe: composite propellant, nano-manganese dioxide, pressure exponent, burning rate
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