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国际能源材料和化学驱动期刊

每年出版 6 

ISSN 打印: 2150-766X

ISSN 在线: 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

INSENSITIVE HIGH ENERGY BOOSTER PROPELLANT SUITABLE FOR HIGH PRESSURE OPERATION

卷 6, 册 4, 2007, pp. 501-510
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v6.i4.60
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摘要

Investigators at the Naval Air Warfare Center Weapons Division (NAWCWD), China Lake, California, have developed a new family of high-energy Class 1.3 booster propellants by utilizing RDX, AP, and AN as the mixed oxidizers and aluminum as the metal fuel. The solid materials were incorporated into HTPE/BuNENA or HTCE/BuNENA binder and the resulting propellant exhibited good processing properties. In addition to desirable combustion properties, these propellants have good safety characteristics, as well as excellent mechanical attributes, that make them suitable to withstand demanding tactical environments. More importantly, these propellants burned at a rate of 0.5 in/s at 1,000 psia (12.7 mm/s at 6.895 MPa) and showed no pressure slope break up to 8,000 psi (55.15 MPa). Due to this desirable combustion characteristic, the potential performance of these propellants could be as much as 10 to 15% higher than that of conventional Class 1.3 HTPB/AP/aluminum propellants if they could be utilized for high-pressure operation.

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