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International Journal of Energetic Materials and Chemical Propulsion

Выходит 6 номеров в год

ISSN Печать: 2150-766X

ISSN Онлайн: 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

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EFFECTS OF CL-20 ON THE PROPERTIES OF GLYCIDYL AZIDE POLYMER (GAP) SOLID ROCKET PROPELLANT

Том 15, Выпуск 1, 2016, pp. 49-64
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2015012094
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Краткое описание

The microstructures and granularity distributions of HMX and CL-20 particles were analyzed. Three industrial and research-type GAP-based solid propellants containing CL-20 particles, featuring the same nominal composition, were prepared and experimentally tested. The effects of CL-20 particles on the rheological properties, energetic properties, and the hazardous properties of GAP-based solid propellants were investigated. The properties mentioned above were also compared to those propellants containing HMX. Also, the strand burning rate and the associated combustion properties of propellants were determined. It turned out that the GAP-based propellants containing CL-20 particles can be prepared and cast safely. GAP-based propellants containing CL-20 particles are more sensitive to impact and friction compared to propellants with HMX. However, the addition of CL-20 particles to the propellant formulation can increase the burning rate and affect the combustion behavior, when compared to the reference propellant.

ЦИТИРОВАНО В
  1. Wang Jiangning, Yang Lilong, Zheng Wei, Zhang Jun, Study on Comparative Performance of CL‐20/RDX‐based CMDB Propellants, Propellants, Explosives, Pyrotechnics, 44, 9, 2019. Crossref

  2. Pang WeiQiang, DeLuca Luigi T., Xu HuiXiang, Wang Ke, Fan XueZhong, Zhao FengQi, Effects of Innovative Insensitive Energetic Materials: 1,1-Diamino-2,2-Dinitroethylene (FOX-7) on the Performance of Solid Rocket Propellants, in Innovative Energetic Materials: Properties, Combustion Performance and Application, 2020. Crossref

  3. Wang Yinglei, An Ting, Yan Ning, Yan Zhengfeng, Zhao Baodong, Zhao Fengqi, Nanochromates MCr2O4 (M = Co, Ni, Cu, Zn): Preparation, Characterization, and Catalytic Activity on the Thermal Decomposition of Fine AP and CL-20, ACS Omega, 5, 1, 2020. Crossref

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