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International Journal of Energetic Materials and Chemical Propulsion

年間 6 号発行

ISSN 印刷: 2150-766X

ISSN オンライン: 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

ASSESSING THE PERFORMANCE OF A GREEN LIQUID FUEL HYPERGOLIC WITH HYDROGEN PEROXIDE IN A 50 N BIPROPELLANT THRUSTER

巻 20, 発行 1, 2021, pp. 21-30
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2020032684
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要約

The last decades have witnessed an increasing interest in the development of green propellants for propulsion systems. Particularly in the low thrust domain, where a feasible alternative to the storable liquid bipropellant system hydrazine - nitrogen tetroxide is yet to be fully demonstrated, the application of green hypergolic propellants such as ethanol and H2O2 90 wt% appears to be a promising one. This work presents the design and firing test of a 50 N bipropellant thruster based on the H2O2 90 wt% − monoethanolamine-ethanol hypergolic pair catalyzed by Cu2+, previously developed by our research group. The 5 s firing test, conducted under a swirl injection scheme, yielded average values of 50.38 N, 147 s, and 1210 m/s for thrust, Isp, and c*, respectively, with the target value of 5 bar for the chamber pressure being reached after 2 s of operation. Alongside with a c* efficiency of 84%, these results suggest that the assessed green hypergolic bipropellant pair may be a promising alternative for applications in the low-thrust range.

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によって引用された
  1. Negri Michele, Lauck Felix, Hot Firing Tests of a Novel Green Hypergolic Propellant in a Thruster, Journal of Propulsion and Power, 38, 3, 2022. Crossref

2002 記事の閲覧数 93 記事のダウンロード 記事の統計
2002 記事の閲覧数 93 記事のダウンロード 1 Crossref 引用数 Google
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