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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 2

SPECIAL ISSUE: KENNETH KUO SECOND MEMORIAL ISSUE
GUEST EDITORS: LUIGI T. DELUCA, KEIICHI HORI, & JOHN F. ZEVENBERGEN

DOI: 10.1615/IntJEnergeticMaterialsChemProp.v16.i2

ADVANCED ENERGETIC MATERIALS AND TECHNIQUES FOR ROCKET PROPULSION: IN HONOR OF PROF. KENNETH KUAN-YUN KUO Luigi T. De Luca, Keiichi Hori, John Zevenbergen
pp. v-xiii
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v16.i2.10
EFFECT OF AZODICARBONAMIDE PARTICLES ON THE REGRESSION RATE OF HYDROXYL-TERMINATED POLYBUTADIENE (HTPB)-BASED FUELS FOR HYBRID ROCKET PROPULSION Suhang Chen, Yue Tang, Wei Zhang, Ruiqi Shen, Luigi DeLuca, Yinghua Ye
pp. 103-114
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018022374
IGNITION AND COMBUSTION CHARACTERISTICS OF A MICRO-ELECTROMECHANICAL SYSTEM (MEMS) PYROTECHNIC THRUSTER FOR MICRO PROPULSION APPLICATIONS Harshit Shukla, Gusain Rajesh Singh Nandan, Priyanka Shukla, Vinod Kumar, Mohan Varma
pp. 115-123
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018024455
EFFECTS OF DIFFERENT DECELERATION AGENTS ON THE PROPERTIES OF HYDROXYL TERMINATED POLYETHER (HTPE)-BASED COMPOSITE SOLID PROPELLANTS Wei Qiang Pang, Jun Qiang Li, Luigi DeLuca, Ke Wang, XiaoLong Fu, Xue Zhong Fan, Huan Li
pp. 125-138
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018025006
IGNITION AND COMBUSTION OF HYDROXYL-TERMINATED POLYBUTADIENE (HTPB)-BASED SOLID FUELS LOADED WITH INNOVATIVE MICROMETER-SIZED METALS Zhao Qin, Christian Paravan, Giovanni Colombo, Feng-qi Zhao, Ruiqi Shen, Jian-hua Yi, Luigi DeLuca
pp. 139-150
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018022772
CYCLIC QUENCHING AND IGNITION OF LOW-STRETCH DIFFUSION FLAMES Gary P. Garbinski, James S. T'ien
pp. 151-163
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018022944
HIGH-TEMPERATURE COATING: HYBRID ROCKET MOTOR THERMAL PROTECTION CASE HISTORY Marcela Galizia Domingues, José Atílio Fritz Fidel Rocco
pp. 165-174
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018023565
COUPLING OF TRANSIENT THERMAL AND MECHANICAL STRESSES COMPUTATIONS IN GRAPHITE NOZZLE MATERIALS Ragini Acharya, Brian Evans, Jonathan Pitt, Francesco Costanzo, Kenneth K. Kuo
pp. 175-195
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018024875
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