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International Journal of Energetic Materials and Chemical Propulsion

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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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COMBUSTION BEHAVIOUR INVESTIGATION OF SOLID FUELS USING A MICRO-SIZED HYBRID ROCKET MOTOR

Том 7, Выпуск 3, 2008, pp. 193-207
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v7.i3.30
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A micro-sized hybrid rocket motor was designed, built, and implemented to investigate the comparative combustion behavior of a variety of solid fuel compositions. The goal of this experimental effort is to obtain a relative grading of different solid fuel formulations in terms of regression rate, ignition delay, and radiation emission. Air and oxygen/nitrogen mixtures (up to 50% of oxygen), injected at the head-end of the micromotor, were used as oxidizer. In this phase of investigation, the average chamber pressure was changed in the range of 3.5 to 13 bar, and the volumetric flow rate, 20 to 60 lpm. Quasi-steady regression rates were measured by a proprietary video technique. Ignition delay testing was carried out by exposing solid fuel samples to a controlled laser radiant flux in the range 100 to 300 W/cm2. Spontaneous radiant energy emission was assessed by means of a microcalorimeter at 7 and 14 bar pressure and 20 and 60 lpm oxidizer flow rate. To validate the effectiveness of the experimental approach, pure HTPB-based fuel was considered in this paper. Some representative data points for aluminized HTPB and paraffin-based fuels are also reported.

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