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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

IGNITION AND COMBUSTION CHARACTERISTICS OF A MICRO-ELECTROMECHANICAL SYSTEM (MEMS) PYROTECHNIC THRUSTER FOR MICRO PROPULSION APPLICATIONS

巻 16, 発行 2, 2017, pp. 115-123
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018024455
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要約

A functional micro-electromechanical system (MEMS)-based micro-thruster using boron–potassium nitrate pyrotechnic composition with an electron beam deposited platinum heater has been characterized for reproducible ignition and sustained combustion. Configuration of the device, assembly process, and the energetic material were selected based on a detailed study involving a series of ignition tests. Successful ignition was achieved for the chosen configuration and the energetic material. The development demonstrated potential of such devices along with scalability for futuristic applications aimed toward downsizing of micro-spacecraft propulsion systems.

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  6. Shukla Harshit, Rajvanshi Tushar, Gupta Tanish, Kumar Vipin, Gaurav Kumar, Kumar Deepak, Diamond based power electronic devices for aerospace application, THE 8TH ANNUAL INTERNATIONAL SEMINAR ON TRENDS IN SCIENCE AND SCIENCE EDUCATION (AISTSSE) 2021, 2659, 2022. Crossref

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