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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

THE INFLUENCE OF SPHERICAL GRANULAR PROPELLANTS ON THE COMBUSTION PROPERTIES OF HIGH-BURNING-RATE PROPELLANT

巻 9, 発行 6, 2010, pp. 467-476
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2011001378
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要約

Novel spherical grain-binding, high-burning-rate propellant is a kind of compound structure propellant (called a consolidated propellant) that is prepared using a spherical granular propellant (spherical propellant grains) as the dispersed phase and a colloidal binder as the continuous phase. The effects of composition, particle-size, and morphology of spherical propellant grains on the combustion performance of propellants were each investigated. The results show that the burning rate of the propellant decreases with the increase of the burning rate of spherical propellant grains. The greater the difference in burning rate between the spherical propellant grains and the binder, the higher the burning rate of the propellant will be. The burning rate of the consolidated propellant increases with a decrease in particle size. When compared with that of propellants prepared with smooth-faced spherical propellant grains, the burning rate of propellants prepared with shaggy spherical propellant grains is much higher; however, combustion can become less stable.

によって引用された
  1. Yavor Yinon, Rosenband Valery, Gany Alon, Reduced agglomeration in solid propellants containing porous aluminum, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 228, 10, 2014. Crossref

  2. Zhang Xi, Li Xiaojiang, Ren Zhi, Chen Jing, Liu Meng, Wu Xiong-Gang, A New Insight of Carbon Blacks and Burning Catalysts in Composite Modified Double Base Propellant, in 2021 International Conference on Development and Application of Carbon Nanomaterials in Energetic Materials, 276, 2022. Crossref

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