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JOURNALS // Fizika Goreniya i Vzryva // Archive

Fizika Goreniya i Vzryva, 2020 Volume 56, Issue 6, Pages 78–84 (Mi fgv723)

This article is cited in 8 papers

Preparation and properties of a flake aluminum powder in an ammonium-perchlorate-based composite modified double-base propellant

D.-Q. Wanga, H.-M. Yua, J. Liua, F.-S. Lia, X.-X. Jinb, S.-J. Zhenga, T.-T. Zhengb, Y. Lic, Z.-J. Zhangb, D. Lic, Z.-G. Lanc

a National Special Superfine Powder Engineering Research Center of China, School of Chemical Engineering, Nanjing University of Science and Technology, 210094, Nanjing, China
b Shanghai Space Propulsion Technology Research Institute, 313000, Huzhou, China
c Shanxi Xing'an Chemical Industry Co. Ltd., Taiyuan, China

Abstract: A flake aluminum powder (F-Al) is prepared by a bi-directional rotation mill method using a spherical aluminum powder (S-Al) as a raw material. Then, these two kinds of aluminum powders are used to prepare ammonium perchlorate-based composite modified double-base (AP-based CMDB) propellants. The properties of two kinds of AP-based CMDB propellants, such as the thermal decomposition performance, mechanical sensitivity, and combustion performance, are comprehensively researched. The results show that the exothermic peak temperature of the F-Al-AP-based CMDB propellant is lower than that of the S-Al-AP-based CMDB propellant. The impact and friction sensitivities of the propellant decrease by 12% and 187% after using F-Al to replace S-Al. In addition, the burning rate of the F-Al-AP-based CMDB propellant is 5.5% higher.

Keywords: AP-based CMDB propellant, aluminum morphology, thermal stability, thermal decomposition, mechanical sensitivity, burning rate.

UDC: 532.5

Received: 17.07.2019
Revised: 25.02.2020
Accepted: 15.05.2020

DOI: 10.15372/FGV20200608


 English version:
Combustion, Explosion and Shock Waves, 2020, 56:6, 691–696

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