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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

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NEW ACTIVE BINDER-BASED PROPELLANTS: A COMPARISON WITH CLASSICAL COMPOSITE AP/HTPB PROPELLANTS

Volume 12, Numéro 1, 2013, pp. 1-13
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2013005271
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RÉSUMÉ

For decades, research activities studying the combustion mechanisms of energetic materials, solid propellants, and their ingredients have been carried out at ONERA. For the past few years, new propellants, including active binders and various energetic oxidizers (octogen, ammonium dinitramide, hexanitrohexaazaisowurtzitane, etc.) with high volumetric impulse potential have been tested. This paper describes the work performed at ONERA and covers the development of the energetic propellants from the understanding of the surface combustion mechanism, using information from visualization techniques to develop a simplified model leading to the burning rate evaluation. The validation of the input data required by the models is of major importance; specific experimental setup and apparatus have been used for determining pertinent parameters. The consistency of these data was verified and is presented in this paper. A comparison between ammonium perchlorate/hydroxyl-terminated polybutadiene composite propellants having an inert binder and the new propellants with active binders shows that the combustion processes of the new propellants differ significantly from those of the classical composite propellants.

CITÉ PAR
  1. Li Ping, Wang Xiaochuan, Study on Nitrile Oxide for Low-Temperature Curing of Liquid Polybutadiene, Materials, 15, 9, 2022. Crossref

  2. Quagliano Amado Javier Carlos, Ross Pablo Germán, Mattos Silva Murakami Lidia, Narciso Dutra Jorge Carlos, Properties of Hydroxyl‐Terminal Polybutadiene (HTPB) and Its Use as a Liner and Binder for Composite Propellants: A Review of Recent Advances, Propellants, Explosives, Pyrotechnics, 47, 5, 2022. Crossref

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