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International Journal of Energetic Materials and Chemical Propulsion

Выходит 6 номеров в год

ISSN Печать: 2150-766X

ISSN Онлайн: 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

DIAGNOSTIC TOOLS FOR STUDIES ON BURN-RATE BEHAVIOR OF ADVANCED SOLID PROPELLANTS

Том 3, Выпуск 1-6, 1994, pp. 634-641
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v3.i1-6.610
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Краткое описание

This paper reports the comparative burn-rate data obtained by Crawford bomb and acoustic emission techniques for double-base (DB) composite modified double-base (CMDB) composite (CP) nitramine-based minimum signature compositions and glycidyl azide prepolymer (GAP) based propellants. The acoustic technique gave higher burn rates for aluminized compositions (CP and CMDB) and lower burn rates in the case of non-aluminized propellants and minimum signature compositions with minor quantities of Al. Results obtained by both techniques were in close agreement for GAP-based compositions. A correlation between strand-burner data and test-motor burn rates has been established during this study to predict rocket motor performance. The effect of mass flow rate on overall ballistic performance has also been evaluated for selected high-energy compositions.

ЦИТИРОВАНО В
  1. ATHAWALE B. K., ASTHANA S. N., SINGH HARIDWAR, Burning Rate Studies of Metal Powder (Ti, Ni)–Based Fuel-Rich Propellants, Journal of Energetic Materials, 22, 2, 2004. Crossref

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