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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

COMBUSTION OF ALANE-BASED SOLID FUELS

Volumen 9, Ausgabe 3, 2010, pp. 249-266
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v9.i3.50
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ABSTRAKT

In this study the combustion behavior of solid fuels loaded with micron-sized aluminum, nanoaluminum, and aluminum hydride with loadings of 10, 20, and 40 mass % are compared directly using pure oxygen as the oxidizer. An opposed flow burner was used to screen the various fuels at various oxidizer flow rates. Regression rates were gathered over oxidizer impingement velocities ranging from approximately 40 to 160 cm/s (strain rates of 80-320 s−1). Fuels loaded with aluminum hydride were found to have regression rates comparable to or better than that of the baseline hydroxyl terminated polybutadiene (HTPB) fuel. In addition, the regression rate increased with increasing aluminum hydride content. Conversely, the regression rates of fuels loaded with micron-sized aluminum were found to decrease with increasing aluminum content. Emission spectroscopy revealed that under most conditions the aluminum in the fuels loaded with micron-sized aluminum did not ignite within the immediate vicinity of the solid fuel sample. Temperature measurements determined from thermal emission support this conclusion as well. Finally, a lab-scale hybrid rocket motor was used to compare the combustion performance of the fuels relative to each other. It was found for the same oxidizer mass flow rate, pressure and thrust were highest for alanized fuels. Data included were thrust, pressure, regression rate, and mass burning rate.

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