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International Journal of Energetic Materials and Chemical Propulsion

Published 6 issues per year

ISSN Print: 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

Volume 16, 2017 Issue 1

DOI: 10.1615/IntJEnergeticMaterialsChemProp.v16.i1

PREFACE: "ADVANCED ENERGETIC MATERIALS AND TECHNIQUES FOR ROCKET PROPULSION" IN HONOR OF PROF. KENNETH KUAN-YUN KUO Luigi DeLuca, Keiichi Hori, John Zevenbergen
pp. v-vii
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v16.i1.10
THANKS FOR THE MEMORIES: REMINISCENCES COLLECTED BY THE CO-EDITORS
pp. ix-xviii
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v16.i1.20
THANKS FOR THE MEMORIES: KEN AT PRINCETON UNIVERSITY (1968–1972) AS SEEN BY LEONARD H. CAVENY
pp. xix-xxi
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v16.i1.30
ASSESSMENT OF THE PERFORMANCE OF ABLATIVE INSULATORS UNDER REALISTIC SOLID ROCKET MOTOR OPERATING CONDITIONS Heath T. Martin, Andrew C. Cortopassi, Kenneth K. Kuo
pp. 1-22
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2017021828
MODELING OF EVOLUTION OF THE COARSE FRACTION OF CONDENSED COMBUSTION PRODUCTS ON A SURFACE OF BURNING ALUMINIZED PROPELLANT AND WITHIN A COMBUSTION PRODUCTS FLOW Valery A. Babuk, Alexander A. Nizyaev
pp. 23-38
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2017021173
TESTING ELECTRIC EFFECTS ON THE BURNING RATE OF AMMONIUM-NITRATE-BASED SOLID PROPELLANTS Inna Zamir, Dan Grinstein, Alon Gany
pp. 39-47
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2017021242
FLAME VISUALIZATION AND COMBUSTION PERFORMANCE OF ENERGETIC PARTICLE EMBEDDED PARAFFIN-BASED FUELS FOR HYBRID ROCKET PROPULSION Yue Tang, Suhang Chen, Wei Zhang, Ruiqi Shen, Luigi DeLuca, Yinghua Ye
pp. 49-59
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2017021530
AMMONIUM DINITRAMIDE/GLYCIDYL AZIDE POLYMER (ADN/GAP) COMPOSITE PROPELLANTS WITH AND WITHOUT METALLIC FUELS Volker Gettwert, Andrea Franzin, Manfred A. Bohn, Luigi DeLuca, Volker Weiser
pp. 61-79
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018021254
FUEL-RICH ALUMINUM−METAL FLUORIDE THERMITES Siva Kumar Valluri, Ian Monk, Mirko Schoenitz, Edward Dreizin
pp. 81-101
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018021842
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