Fizika Goreniya i Vzryva
RUS  ENG    JOURNALS   PEOPLE   ORGANISATIONS   CONFERENCES   SEMINARS   VIDEO LIBRARY   PACKAGE AMSBIB  
General information
Latest issue
Archive

Search papers
Search references

RSS
Latest issue
Current issues
Archive issues
What is RSS


Fizika Goreniya i Vzryva:
Year:
Volume:
Issue:
Page:
Find




Personal entry:
Login:
Password:
Save password
Enter
Forgotten password?
Register

Fizika Goreniya i Vzryva, 2020, Volume 56, Issue 6, Pages 78–84
DOI: https://doi.org/10.15372/FGV20200608 (Mi fgv723) 		 
This article is cited in 8 scientific papers (total 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
Citations (8)
DOI: https://doi.org/10.15372/FGV20200608
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.
Funding agency Grant number
National Natural Science Foundation of China 51606102
Received: 17.07.2019
Revised: 25.02.2020
Accepted: 15.05.2020
English version:
Combustion, Explosion and Shock Waves, 2020, Volume 56, Issue 6, Pages 691–696
DOI: https://doi.org/10.1134/S0010508220060088
Bibliographic databases:
Document Type: Article
UDC: 532.5
Language: Russian
Citation: D.-Q. Wang, H.-M. Yu, J. Liu, F.-S. Li, X.-X. Jin, S.-J. Zheng, T.-T. Zheng, Y. Li, Z.-J. Zhang, D. Li, Z.-G. Lan, “Preparation and properties of a flake aluminum powder in an ammonium-perchlorate-based composite modified double-base propellant”, Fizika Goreniya i Vzryva, 56:6 (2020), 78–84; Combustion, Explosion and Shock Waves, 56:6 (2020), 691–696
Citation in format AMSBIB
\Bibitem{WanYuLiu20}
\by D.-Q.~Wang, H.-M.~Yu, J.~Liu, F.-S.~Li, X.-X.~Jin, S.-J.~Zheng, T.-T.~Zheng, Y.~Li, Z.-J.~Zhang, D.~Li, Z.-G.~Lan
\paper Preparation and properties of a flake aluminum powder in an ammonium-perchlorate-based composite modified double-base propellant
\jour Fizika Goreniya i Vzryva
\yr 2020
\vol 56
\issue 6
\pages 78--84
\mathnet{http://mi.mathnet.ru/fgv723}
\crossref{https://doi.org/10.15372/FGV20200608}
\elib{https://elibrary.ru/item.asp?id=44480681}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2020
\vol 56
\issue 6
\pages 691--696
\crossref{https://doi.org/10.1134/S0010508220060088}
Linking options:
  • https://www.mathnet.ru/eng/fgv723
  • https://www.mathnet.ru/eng/fgv/v56/i6/p78
    • This publication is cited in the following 8 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    		Fizika Goreniya i Vzryva Fizika Goreniya i Vzryva
    Statistics & downloads:
    Abstract page:33
     
      Contact us:
    		  Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2024