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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

Indexed in

CONTAINED LOW PRESSURE COMBUSTION OF NIKE AND IMPROVED HAWK ROCKET MOTORS: EXPERIMENTAL TECHNIQUES AND EMISSIONS MEASUREMENTS

Volume 5, Numéro 1-6, 2002, pp. 40-49
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.60
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RÉSUMÉ

Results obtained from three rocket motor propellant burn tests conducted in a large, sealed, underground cavern are described. These tests made use of a runnel complex at the U.S. Department of Energy's Nevada Test Site, Mercury, NV, USA. The NIKE rocket motor containing double base propellant was used in two tests (two and four motors, respectively), and a third test used two Improved HAWK rocket motors containing composite propellant. In each test, relatively small quantities of explosive were used to initiate non-propulsive propellant bums that lasted approximately 20 seconds. An extensive suite of both time-resolved and time-averaged data was collected for several hours after each test. These data include pressure and temperature transients in the test chamber as well as concentrations and compositions of the gas species and aerosols generated by the combustion process.

CITÉ PAR
  1. Koch Ernst‐Christian, Insensitive High Explosives: V. Ballistic Properties and Vulnerability of Nitroguanidine Based Propellants, Propellants, Explosives, Pyrotechnics, 46, 2, 2021. Crossref

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