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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

COMBUSTION CHARACTERISTICS OF HYDROXYLAMMONIUM NITRATE AQUEOUS SOLUTIONS

巻 9, 発行 3, 2010, pp. 219-231
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v9.i3.30
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要約

Hydroxylammonium nitrate (HAN) based liquid propellant has been investigated as a candidate for the monopropellant to be utilized in the reaction control system of satellites as an alternative to hydrazine. This propellant, which consists of ammonium nitrate, methanol, and water, has moderate burning characteristics, sufficiently low freezing temperature, high density, low toxicity, and its density × Isp is 70% higher than hydrazine. In a previous study, the combustion characteristics of the propellants were obtained and found to be very complex. In this paper, the research was focused on the combustion characteristics of HAN aqueous solution. Sample solutions of several concentrations, 95-50 mass %, were prepared. The measurement of linear burning rates, the temperature measurement of the combustion wave, and the observation of combustion phenomena were included in the study. The linear burning rate does not increase monotonically with increasing HAN concentration. The burning rates increase as the HAN concentration increases up to 80 mass %, and decrease as the concentration increases from 80 to 95 mass %. The burning rate peaks at around 80 mass % of HAN concentration. The combustion mode is very complex and is dependent upon composition and pressure. Temperature measurements indicate that the role of the two-phase region is very important, and the boiling of water caused by superheat is responsible for the high burning rate. The relationship between the rate of nucleation of bubbles and the linear burning rate is discussed.

によって引用された
  1. Katsumi T., Inoue T., Nakatsuka J., Hasegawa K., Kobayashi K., Sawai Sh., Hori K., HAN-based green propellant, application, and its combustion mechanism, Combustion, Explosion, and Shock Waves, 48, 5, 2012. Crossref

  2. Wei Li, Yang Xiang, Bi-feng Zhang, Song Wang, Jun Liu, Qing-guo Lin, Jun Yang, Degradation of CVD-SiC coated C/SiC composites exposed to the monopropellant combustion products based on Hydroxylammonium nitrate (HAN), Corrosion Science, 74, 2013. Crossref

  3. Hori Keiichi, Lessons Learned in the Thruster Tests of HAN, in Chemical Rocket Propulsion, 2017. Crossref

  4. Atamanov M., Amrousse R., Jandosov J., Hori K., Kerimkulova A., Chenchik D., Kolesnikov B., Combustion Characteristics of HAN-based Green Propellant Assisted with Nanoporous Active Carbons, Eurasian Chemico-Technological Journal, 19, 3, 2017. Crossref

  5. Esparza Alan A., Shafirovich Evgeny, Thermoanalytical Study of Hydroxylammonium Nitrate Decomposition at High Pressures, AIAA Propulsion and Energy 2019 Forum, 2019. Crossref

  6. Mansurov Zulkhair A., Amrousse Rachid, Hori Keiichi, Atamanov Meiram K., Combustion/Decomposition Behavior of HAN Under the Effects of Nanoporous Activated Carbon, in Innovative Energetic Materials: Properties, Combustion Performance and Application, 2020. Crossref

  7. Wang Xin, Yang Tao, Li Qingyu, Yan Peng, Wang Shaopeng, Comparative study of failure mechanisms of MoSi2 coating on Mo1 wire mesh under isothermal oxidation and hot-fire test using a hydroxylammonium nitrate based monopropellant, Journal of the European Ceramic Society, 41, 4, 2021. Crossref

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