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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

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BURNING-RATE CHARACTERISTICS OF BORON/[BAMO/NMMO] FUEL-RICH SOLID PROPELLANT UNDER BROAD RANGES OF PRESSURE AND TEMPERATURE

巻 2, 発行 1-6, 1993, pp. 412-426
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v2.i1-6.250
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要約

Burning-rate characteristics of pure and 10% boron-based 3,3-bis (azido- methyl) oxetane (BAMO), and 3-nitratomethyl 3-methyl oxetane (NMMO) copolymer fuel-rich solid propellants in air atmosphere have been studied using a pressure and temperature controlled test chamber with optical windows. The temperature and pressure ranges of test firings were −10 to 60°C and 240.5 to 1030.6 KPa (35 to 150 psia), respectively. Temperature sensitivity of the burning rate, one of the most important design parameters in practical application to solid-fuel ramjets (SFRJ) and to solid-propellant ducted rockets (SDR), was deduced from the experimental data. The thermal wave structure of boron/[BAMO/NMMO] copolymer fuel-rich solid propellants under no cross flow conditions was measured by fine-wire thermocouples. From the temperature-time traces recorded at a fixed chamber pressure, the burning surface temperature was found to increase with the initial temperature. Furthermore, the combustion residues of boron/[BAMO/NMMO] copolymer samples, recovered from the tests with different initial temperatures, were examined employing a scanning electron microscope.

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  1. GUO Yang, ZHANG Wei, ZHOU Xing, DENG Lei, Oxidation Characteristics of Magnesium Diboride, Journal of Inorganic Materials, 34, 8, 2019. Crossref

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