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International Journal of Energetic Materials and Chemical Propulsion

Publication de 6  numéros par an

ISSN Imprimer: 2150-766X

ISSN En ligne: 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 ALUMINUM-BASED MUTLIMETAL PARTICLES ON SOLID PROPELLANTS

Volume 19, Numéro 1, 2020, pp. 1-9
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2019028001
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RÉSUMÉ

Aluminum is well known to increase the specific impulse of composite propellants due to a higher adiabatic flame temperature associated with it. Aluminized propellants typically produce large agglomerates on the burning surface of solid propellants. These agglomerates are the main drawback of using aluminum in composite solid propellants, as they give rise to two-phase flow losses and slag accumulation, resulting in as much as 10% reduction in specific impulse. Nanosized aluminum powder enhances the burning rate of solid propellants significantly; however, the oxide content in it is much higher than micron-aluminum due to its considerable specific surface. This paper discusses an experimental investigation focused on the effects of micron-sized AlMg on the combustion behavior of solid propellants. Combustion characteristics and combustion condensed particles of solid propellants loaded with AlMg were investigated here. The results show that AlMg is more effective than Al in increasing the burning rate of hydroxyl-terminated polybutadiene based propellant since much heat was released with the help of the reaction between Al and Mg. The particle size of condensed combustion particles was reduced greatly thanks to the use of AlMg.

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