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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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SICOMIN-ROT K 3130 S AS A BURNING RATE MODIFIER

Том 5, Выпуск 1-6, 2002, pp. 236-243
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.250
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Краткое описание

Effect of one new burning-rate modifier with trademark Sicomin-Rot K3130 S was studied, to determine its influence on propellant burning rate. Examination of its influence on combustion has been performed on composite solid rocket propellants series known as Flexolite. All Flexolite-series of propellants are based on ammonium perchlorate as oxidizer, and modified polyvinyl chloride as binder. Its effect as catalyst is shown on both non-aluminized and aluminized formulations, and compared with other catalysts. It was shown that burning-rate modifier has a substantial effect upon the burning rate, increasing it in dependence of its amount in propellant formulation. Also, influence of plasticizers on propellant burning rate of non-aluminized propellant with a new burning-rate modifier is shown. All burning rates were measured in a special test motor at different pressures, using small-motor measurement method.

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