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International Journal of Energetic Materials and Chemical Propulsion

Published 6 issues per year

ISSN Print: 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

COMBUSTION STUDY OF BORON-BASED FUEL-RICH SOLID PROPELLANT

Volume 2, Issue 1-6, 1993, pp. 375-385
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v2.i1-6.220
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ABSTRACT

This paper presents results of the theoretical and experimental studies on combustion behaviors of boron-based fuel-rich solid propellants. Nonequilibrium temperature (T") calculations and theoretical performance predictions regarding a baseline formulation and five candidate propellants reveled promising aspects for ramrocket application. Both amorphous boron and crystalline boron that coated with GAP or LiF were incorporated in these propellants. The detailed thermochemical behaviors of the boron fuel-rich propellants and their major ingredients were investigated by thermal analyzer. Fine-wire thermocouple, color high-speed video system, powder diffractometer, strand burner, and QPCB were also employed in this studies. All data confirmed the effects of both coatings on decomposition and combustion phenomena of boron propellants, although LiF-coated boron is more effective than GAP-coated boron, and amorphous boron burned more readily than crystalline boron.

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