N. S. Belousova, O. G. Glotov, A. V. Gus'kov, “Study of the additive modifiers effect on the combustion characteristics of composite propellants with aluminium”, Chelyab. Fiz.-Mat. Zh., 9:2 (2024), 195

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Chelyabinskiy Fiziko-Matematicheskiy Zhurnal, 2024, Volume 9, Issue 2, Pages 195–202
DOI: https://doi.org/10.47475/2500-0101-2024-9-2-195-202 (Mi chfmj370)

Dynamics of Multiphase Media

Study of the additive modifiers effect on the combustion characteristics of composite propellants with aluminium

N. S. Belousova^ab, O. G. Glotov^ab, A. V. Gus'kov^a

^a Novosibirsk State Technical University, Novosibirsk, Russia
^b Voevodsky Institute of Chemical Kinetics and Combustion SB RAS, Novosibirsk, Russia

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DOI: https://doi.org/10.47475/2500-0101-2024-9-2-195-202

Abstract: We studied the effect of modifier additives TiB

$_2$ , AlMgB

$_{14}$ , (NH

$_4$ )

$_2$ TiF

$_6$ , NH

$_4$ BF

$_4$ , Ca

$_3$ (PO

$_4$ )

$_2$ on the combustion parameters of composite propellants based on aluminum powder as a fuel (about 20 % wt.), ammonium perchlorate as an oxidizer (about 60 % wt.), and energetic binder (MPVT about 20 % wt.). As a result of the study, the influence of additives on the rate of composite propellants combustion, dimensionless mass and agglomerate size was revealed.

Keywords: composite propellants, aluminum, additives, titanium diboride, aluminum-magnesium boride, ammonium tetrafluoroborate, ammonium-titanium fluoride, 3-substituted calcium phosphate, combustion rate, agglomeration, condensed combustion products, particle size distribution.

Received: 11.12.2023
Revised: 26.03.2024

Document Type: Article

UDC: 536.46

Language: Russian

Citation: N. S. Belousova, O. G. Glotov, A. V. Gus'kov, “Study of the additive modifiers effect on the combustion characteristics of composite propellants with aluminium”, Chelyab. Fiz.-Mat. Zh., 9:2 (2024), 195–202

Citation in format AMSBIB

\Bibitem{BelGloGus24}

\by N.~S.~Belousova, O.~G.~Glotov, A.~V.~Gus'kov

\paper Study of the additive modifiers effect on the combustion characteristics of composite propellants with aluminium

\jour Chelyab. Fiz.-Mat. Zh.

\yr 2024

\vol 9

\issue 2

\pages 195--202

\mathnet{http://mi.mathnet.ru/chfmj370}

\crossref{https://doi.org/10.47475/2500-0101-2024-9-2-195-202}

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