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Comparative ballistic efficiency of solid composite propellants: which plasticizer/polymer combination is the energetically preferred binder?

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Lempert D. B., Kazakov A. I., Sheremetev A. B. Comparative ballistic efficiency of solid composite propellants: which plasticizer/polymer combination is the energetically preferred binder? // Mendeleev Communications. 2022. Vol. 32. No. 5. pp. 601-603.
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Lempert D. B., Kazakov A. I., Sheremetev A. B. Comparative ballistic efficiency of solid composite propellants: which plasticizer/polymer combination is the energetically preferred binder? // Mendeleev Communications. 2022. Vol. 32. No. 5. pp. 601-603.
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TY - JOUR
DO - 10.1016/j.mencom.2022.09.010
UR - https://mendcomm.colab.ws/publications/10.1016/j.mencom.2022.09.010
TI - Comparative ballistic efficiency of solid composite propellants: which plasticizer/polymer combination is the energetically preferred binder?
T2 - Mendeleev Communications
AU - Lempert, David Borisovich
AU - Kazakov, Anatoly Ivanovich
AU - Sheremetev, Aleksei Borisovich
PY - 2022
DA - 2022/09/05
PB - Mendeleev Communications
SP - 601-603
IS - 5
VL - 32
ER -
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@article{2022_Lempert,
author = {David Borisovich Lempert and Anatoly Ivanovich Kazakov and Aleksei Borisovich Sheremetev},
title = {Comparative ballistic efficiency of solid composite propellants: which plasticizer/polymer combination is the energetically preferred binder?},
journal = {Mendeleev Communications},
year = {2022},
volume = {32},
publisher = {Mendeleev Communications},
month = {Sep},
url = {https://mendcomm.colab.ws/publications/10.1016/j.mencom.2022.09.010},
number = {5},
pages = {601--603},
doi = {10.1016/j.mencom.2022.09.010}
}
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Lempert, David Borisovich, et al. “Comparative ballistic efficiency of solid composite propellants: which plasticizer/polymer combination is the energetically preferred binder?.” Mendeleev Communications, vol. 32, no. 5, Sep. 2022, pp. 601-603. https://mendcomm.colab.ws/publications/10.1016/j.mencom.2022.09.010.

Keywords

binder
effective impulse
plasticizer
polymer
solid composite propellant
specific impulse

Abstract

The relative efficacy of real energetic plasticizers and polymers for model solid composite propellants comprising 25% aluminum hydride, 50% dinitramide ammonium salt and 25% binder (20% a plasticizer and 5% a polymer) has been estimated. The quantitative dependence of the efficiency of plasticizers on the value of their enthalpy of formation ΔHt0, the oxygen coefficient α, percentage of hydrogen %H and density d has been revealed. 3,4-Dinitrofurazan tested as a plasticizer for the binder provides effective impulse values at the 3rd stage up to ∼2 s higher than those for other plasticizers.

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