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Aluminized Solid Propellants Loaded with Metals and Metal Oxides: Characterization, Thermal Behavior, and Combustion Full article

Source Innovative Energetic Materials: Properties, Combustion Performance and Application
Monography, Springer Nature. Singapore.2020. 547 c. ISBN 9789811548314.
Output data Year: 2020, Pages: 157-182 Pages count : 26 DOI: 10.1007/978-981-15-4831-4
Tags Metal, Metal oxide, Nanopowder, Cyclic nitramines, Burning rate, Propellant
Authors Gromov Alexander A. 1 , Slusarsky Konstantin V. 1,2 , Sergienko Alexey V. 1 , Popenko Elena M. 1 , Dzidziguri Ella L. 1 , Larionov Kirill B. 1,2 , Mishakov Ilya V. 1,3
Affiliations
1 National University of Science and Technology MISiS
2 National Research Tomsk Polytechnic University
3 Boreskov Institute of Catalysis, Russian Academy of Science

Funding (2)

1 Council for Grants of the President of the Russian Federation НШ-2513.2020.8
2 Ministry of Science and Higher Education of the Russian Federation 075-00268-20-02 (0718-2020-0040)(АААА-А20-120070890064-3)

Abstract: In this chapter, the combustion behavior of multicomponent aluminized propellants loaded with different metals and metal oxides (in particular, B, Zn, Ni, Cu, Mo, Co3O4, V2O5, MnO2, Fe2 O3, and CuO) are described. The correlation between properties of propellant composition and components and regularities of burning process are presented for formulations based on mixture of HMX, CL-20, and ammonium perchlorate. The burning law was defined experimentally by means of Vielle bomb over the pressure range 1–10 MPa, while some combustion properties were obtained theoretically. The effects of metal powder chemical and phase composition on burning law were considered as well as their oxidation reactivity, morphological, and the other properties. The most significant increasing of burning rate was observed for substances promoting catalytic propellant components decomposition with nearly constant thermodynamic properties. Thus, addition of metal and metal oxide could be effective way to adjust burning rate of propellants without affecting its ballistic properties.
Cite: Gromov A.A. , Slusarsky K.V. , Sergienko A.V. , Popenko E.M. , Dzidziguri E.L. , Larionov K.B. , Mishakov I.V.
Aluminized Solid Propellants Loaded with Metals and Metal Oxides: Characterization, Thermal Behavior, and Combustion
Monography chapter Innovative Energetic Materials: Properties, Combustion Performance and Application. – Springer Nature., 2020. – C.157-182. – ISBN 9789811548314. DOI: 10.1007/978-981-15-4831-4 OpenAlex OpenAlex
Identifiers:
OpenAlex: W4253406931 | W3038517416
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