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International Journal of Energetic Materials and Chemical Propulsion

年間 6 号発行

ISSN 印刷: 2150-766X

ISSN オンライン: 2150-7678

The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 0.7 To calculate the five year Impact Factor, citations are counted in 2017 to the previous five years and divided by the source items published in the previous five years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) 5-Year IF: 0.7 The Immediacy Index is the average number of times an article is cited in the year it is published. The journal Immediacy Index indicates how quickly articles in a journal are cited. Immediacy Index: 0.1 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.00016 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.18 SJR: 0.313 SNIP: 0.6 CiteScore™:: 1.6 H-Index: 16

Indexed in

COMPARATIVE INVESTIGATION OF DIFFERENT NANO-METAL MATERIALS ON COMBUSTION PROPERTIES OF DB AND CMDB PROPELLANTS

巻 16, 発行 3, 2017, pp. 219-229
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018024804
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要約

In order to understand the effects of different nano-metal materials on the combustion properties of double-base (DB) and composite-modified double-base (CMDB) propellants, five different nanometal (nm) powders including nano-silver (nm-Ag), nano-copper (nm-Cu), nano-nickel (nm-Ni), nano-titanium (nm-Ti), and nano-aluminum (nm-Al) were selected and their effects on the combustion properties of DB and CMDB propellants were investigated. The results show that the five aforementioned nano-materials can enhance the combustion performance of DB and CMDB propellants. The burning rates of DB propellant at 10 MPa, which is the working pressure of many solid rockets, are in the following order: unm - Al > unm - Cu > unm - Ni = unm - Ti > unm - Ag > ublank; the pressure exponents of RDX-CMDB propellant at 6–10 MPa are in the following order: nnm - Ni < nnm - Ag < nnm - Ti < nnm - Cu < nblank < nnm - Al. In particular, 0.6% of nm-Ni can reduce the pressure exponent of RDX-CMDB propellant evidently from 0.26 to - 0.02 at 6-10 MPa, and that nm-Al is effective in increasing the burning rate of DB propellant. In the presence of 0.6% of nm-Al, the burning rate at 10 MPa is increased from 17.12 to 25.84 mm/s, and the pressure exponent at 10–20 MPa is decreased from 0.61 to 0.16.

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  1. Yao Ergang, Xu Siyu, Zhao Fengqi, Huang Taizhong, Li Haijian, Zhao Ningning, Yi Jianhua, Yang Yanjing, Wang Changjian, Study on Thermal Decomposition Behavior, Gaseous Products, and Kinetic Analysis of Bis-(Dimethylglyoximato) Nickel(II) Complex Using TG-DSC-FTIR-MS Technique, Catalysts, 10, 3, 2020. Crossref

  2. Zhao Ying, Zhao Feng-Qi, Xu Si-Yu, Ju Xue-Hai, Molecular reaction dynamics simulation of thermal decomposition for aluminiferous RDX composites, Computational Materials Science, 177, 2020. Crossref

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