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International Journal of Energetic Materials and Chemical Propulsion

Выходит 6 номеров в год

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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BURNING RATE CHARACTERIZATION OF OXSOL LIQUID OXIDIZER

Том 5, Выпуск 1-6, 2002, pp. 563-575
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.590
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Краткое описание

Characterization of the burning behavior of OXSOL liquid oxidizer (70% HAN, 15% AN, and 15% H2O by weight) was performed in transparent test tubes in a windowed liquid propellant strand burner. The burn rate of OXSOL was deduced from the regression history of the liquid surface. The burn rate was found to be a function of test tube diameter and ranged from 40 to 550 mm/s for the pressure range of 2.5 to 20 MPa. OXSOL exhibited two slope breaks with a pressure exponent near 2.9 for 2.5<P<5 MPa, 0.4 for 5<P<9 MPa, and −0.8 for P<9 MPa. The effect of tube diameter on the burning rate of OXSOL is believed to be due to hydrodynamic instability of the burning surface. Additionally, the combustion product gas temperatures were measured to range from 500−650 K as a function of pressure. The burning rate slope break at 5 MPa was found to be very close to the slope break at 5.5 MPa in the plot of the ratio of heat of vaporization to the boiling point of water versus pressure. This similarity in slope break implies the importance of the water vaporization process in the low-pressure combustion of OXSOL. According to Levich's stability analysis, the influence of liquid viscosity and gravity is stabilizing. Without a sufficient level of liquid viscosity to stabilize the liquid burning surface, the planar burning of OXSOL is intrinsically unstable for the test conditions studied.

ЦИТИРОВАНО В
  1. Littler Matthew G., Risha Grant A., Moore Jeffrey D., Yetter Richard A., Boyer J. Eric, Development and Testing of Liquid Simulants, Journal of Propulsion and Power, 37, 4, 2021. Crossref

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