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International Journal of Energetic Materials and Chemical Propulsion

Publicado 6 números por año

ISSN Imprimir: 2150-766X

ISSN En Línea: 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

T-BURNER RESPONSE ANALYSIS USING THE SPP/SSP CODE

Volumen 5, Edición 1-6, 2002, pp. 918-926
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.930
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SINOPSIS

This paper presents the results of a study to compare the stability results of the SPP/SSP code to actual T-Burner experimental data. The SPP/SSP code is the standard solid rocket motor performance program coupled to the Standard Stability Program. Four unique propellants were compared. Two were reduced smoke and two were metallized propellants. Pressure coupled response data was already available for these propellants. This experimental data was evaluated by the T-burner. For the metallized propellants, aluminum oxide particle analysis was also previously performed on the combustion products. The stability analysis was performed using the three- dimensional grain design and ballistic modules and the one dimensional stability module. Types of driving and damping mechanisms included in the analysis included pressure coupling, wall damping and for the metallized propellants, particle damping. The total predicted stability was then compared against the decay and/or growth measured in the T-Burner during a test. The results were surprising in that both the magnitude and trends in the analysis were verified by the data.

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