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Effect of titanium dioxide on the burning rate and agglomeration parameters of aluminized composite propellant Full article

Journal FirePhysChem
ISSN: 2667-1344
Output data Year: 2026, DOI: 10.1016/j.fpc.2026.01.017
Tags Composite propellants, Aluminum, Burning rate, Burning modifier additive, Titanium dioxide, Condensed combustion products, Agglomerates
Authors Glotov Oleg.G. 1,2 , Belousova Natalya S. 1,2 , Sorokin Ivan V. 2 , Makarova Angelina A. 1,2 , Surodin Grigory S. 2 , Yunoshev Alexander S. 3
Affiliations
1 Novosibirsk State Technical University Novosibirsk, 630073, Russia
2 Voevodsky Institute of Chemical Kinetics and Combustion Siberian Branch of the Russian Academy of Sciences, Novosibirsk, 630090, Russia
3 Lavrent'ev Institute of Hydrodynamics Siberian Branch of the Russian Academy of Sciences, Novosibirsk, 630090, Russia

Abstract: The combustion characteristics of composite propellants based on ammonium perchlorate, aluminum powder, active binder, and optionally a modifier additive – titanium dioxide of various types in an amount of 1.5%, were studied experimentally at pressures of 0.35 MPa in nitrogen and 0.1 MPa in air. The burning rate, particle size and morphological composition the condensed combustion products were determined. The types of TiO2 powders were obtained from different manufacturers. One of them was produced by the authors in a combustion mode. It has been established that the use of some TiO2 powders leads decrease in the mass of agglomerates, and to an increase in the burning rate in air. These powders are recommended for further research under a broader range of conditions.
Cite: Glotov O.G. , Belousova N.S. , Sorokin I.V. , Makarova A.A. , Surodin G.S. , Yunoshev A.S.
Effect of titanium dioxide on the burning rate and agglomeration parameters of aluminized composite propellant
FirePhysChem. 2026. DOI: 10.1016/j.fpc.2026.01.017 OpenAlex
Dates:
Submitted: Nov 13, 2025
Accepted: Jan 28, 2026
Published online: Jan 29, 2026
Identifiers:
≡ OpenAlex: W7126020415
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