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International Journal of Energetic Materials and Chemical Propulsion

Erscheint 6 Ausgaben pro Jahr

ISSN Druckformat: 2150-766X

ISSN Online: 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

FERRITE: POTENTIAL NANO-MODIFIER FOR ROCKET PROPELLANTS

Volumen 16, Ausgabe 4, 2017, pp. 337-346
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018013434
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ABSTRAKT

Composite solid propellants were prepared with nano-ferrites, where the nano-ferrites Zn, Mn, Ni, Co, and Cu were used as catalysts. The nano-ferrites were prepared using the chemical co-precipitation method. The catalytic properties of these nanomaterials were measured by thermogravimetric and differential thermal analyses on an ammonium perchlorate/hydroxyl-terminated polybutadiene–based propellant. The experimental results showed an increase in the thermal decomposition of the propellants in the presence of nano-ferrites. The activation energy of the high-temperature decomposition step of the propellants was calculated using the Kissinger equation. The burning rates of the propellants were also measured.

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