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International Journal of Energetic Materials and Chemical Propulsion

Publication de 6  numéros par an

ISSN Imprimer: 2150-766X

ISSN En ligne: 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

STUDY OF THE COMBUSTION MECHANISM OF AN-BASED PROPELLANTS

Volume 7, Numéro 2, 2008, pp. 153-170
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v7.i2.50
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RÉSUMÉ

This paper discusses results obtained in studying the combustion mechanism of ammonium nitrate (AN)-based propellants. For this purpose, a row of progressively complicated AN-based systems: AN/catalyst; AN/catalyst/binder; AN/catalyst/binder/ammonium perchlorate (AP); and AN/catalyst/binder/AP/Al has been studied. It was shown that successive addition of AP and Al to the binary mixture of a catalyzed AN/binder yields a regular increase in the burning rate, accompanied by a small change in the pressure exponent. On the basis of flame structure investigation, it has been determined that the surface temperature of catalyzed AN as well as AN-based propellants is controlled by the dissociative evaporation of the salt. Analysis of obtained results allows for the suggestion of a combustion mechanism for AN-based propellants, which is based on the leading role of heat release in the condensed phase.

CITÉ PAR
  1. Kohga Makoto, Handa Saori, Thermal Decomposition Behaviors and Burning Characteristics of Composite Propellants Prepared Using Combined Ammonium Perchlorate/Ammonium Nitrate Particles, Journal of Energetic Materials, 36, 1, 2018. Crossref

  2. Kohga Makoto, Thermal Decomposition Behavior and Burning Characteristics of Ammonium Nitrate/Polytetrahydrofuran Propellants with Glycerol Propoxylate as a Crosslinking Agent, AIAA Propulsion and Energy 2019 Forum, 2019. Crossref

  3. Sinditskii V. P., Egorshev V. Yu., Serushkin V. V., Filatov S. A., Combustion of energetic materials controlled by condensed-phase reactions, Combustion, Explosion, and Shock Waves, 48, 1, 2012. Crossref

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