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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

BALLISTIC AND COMBUSTION PROPERTIES OF HIGH-PRESSURE EXPONENT HYDROCARBON-BASED FUEL-RICH PROPELLANTS

Volumen 5, Ausgabe 1-6, 2002, pp. 1048-1058
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1070
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ABSTRAKT

The ballistic properties of hydrocarbon-based fuel-rich propellants can be manipulated by various methods. Incorporating fine AP and large surface area ferric oxide particles can substantially increase the burning rate. Alternative oxidizers like KP and RDX can lower the burning rate. Studies showed that the burning rate measurements are highly dependent on three measuring techniques: optical bomb, strand burner and BEM test motors. Pictures of burning fuel-rich propellant showed the formation of a thick porous zone during combustion. The flame temperature of fuel-rich propellants measured with visible spectroscopy differs from values calculated with thermodynamic calculations.

REFERENZIERT VON
  1. Ndizihiwe Prosper, Mkandawire Burnet , Kayibanda Venant , Variation of the Air-Fuel Ratio with Inlet Pressure, Temperature and Density, Advances in Science, Technology and Engineering Systems Journal, 6, 2, 2021. Crossref

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