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International Journal of Energetic Materials and Chemical Propulsion

Выходит 6 номеров в год

ISSN Печать: 2150-766X

ISSN Онлайн: 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

A LOW TEMPERATURE CO-FIRED CERAMIC ELECTROLTYIC MICROTHRUSTER

Том 8, Выпуск 4, 2009, pp. 357-371
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v8.i4.80
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Краткое описание

Liquid monopropellant microthrusters utilizing electrolytic ignition were designed, fabricated, and analyzed. Low temperature co-fired ceramic tape technologies were used initially to fabricate microscale burners in order to evaluate the applicability of the technology to high temperature combustion systems. Microscale diffusion flames were stabilized in the burners, and optical spectroscopy measurements were performed to characterize the flame behavior. The low temperature co-fired ceramic tape technologies were then applied to the fabrication of microthrusters. The microthrusters had integrated silver electrodes to enable ignition of hydroxylammonium nitrate-based liquid monopropellants by electrolytic decomposition. The volume of the thruster combustion chamber was 0.82 mm3. The microthruster was successfully ignited, and a thrust output of approximately 200 mN was measured with a voltage input of 45 V. Energy input as small as 1.9 J was achieved for ignition, and ignition delay as short as 224.5 ms was recorded.

ЛИТЕРАТУРА
  1. Yetter, R.A., Yang, V., Wu, M.H., Wang, Y., Milius, D., Aksay, I.A., and Dryer, F.L., Combustion Issues and Approaches for Chemical Microthrusters.

  2. Risha, G.A., Yetter, R.A., and Yang, V., Electrolytic Ignition of HAN-Based Liquid Propellants.

  3. Risha, G.A., Yetter, R.A., Yang, V., and Fedorczyk, D.A., Fundamental Studies on Electrolytic Ignition of Advanced HAN-Based Liquid Propellants for Space Propulsion Systems.

  4. Zhang, K.L., Chou, S.K., and Ang, S.S., MEMS-Based Solid Propellant Microthruster Design, Simulation, Fabrication, and Testing.

  5. Lewis, D.H., Janson, S.W., Cohen, R.B., and Antonsson, E.K., Digital Micropropulsion.

  6. London, A.P., Ayon, A.A., Epstein, A.H., Spearing, S.M., Harrison, T., Peles, Y., and Kerrebrock, J.L., Microfabrication of a High Pressure Bipropellant Rocket Engine.

  7. Yetter, R.A., Yang, V., Wang, Z., Wang, Y., Milius, D., Peluse, M., Aksay, I.A., Angioletti, M., and Dryer, F.L., Development of Meso and Micro Scale Liquid Propellant Thrusters.

  8. Wu, M.H., Development and Experimental Analyses of Meso and Micro Scale Combustion Systems.

  9. Miesse, C.M., Masel, R.I., Short, M., and Shannon, M.A., Diffusion Flame Instabilities in a 0.75mm Non-Premixed Microburner.

  10. Moll, A.J., Microsystems and Microfluidics: Why not LTCC?.

  11. Golonka, L.J., Zawada, T., Radojewski, J., Roguszczak, H., and Stefanow, M., LTCC Microfluidic System.

  12. Okamasa, T., Lee, G.G., Suzuki, Y., Kasagi, N., and Matsuda, S., Development of a Micro Catalytic Combustor Using High-Precision Ceramic Tape Casting.

  13. Plumlee, D., Steciak, J., and Moll, A., Development of an Embedded Hydrogen Peroxide Catalyst Chamber in Low Temperature Co-Fired Ceramics.

  14. Zhang, K.L., Chou, S.K., and Ang, S.S., Development of a Low-Temperature Co-Fired Ceramic Solid Propellant Microthrusters.

  15. Wu, M.H., Yetter, R.A., and Yang, V., A LTCC Burner for Studying Sub-Millimeter Scale Flames.

  16. Leminski, R.E.B., Simoes, E.W., Furlan, R., Ramos, L., Gongora-Rubio, M.R., Morimoto, N., and Satiago-Aviles, J.J., Development of Microfluidic Devices Using LTCC Substrates.

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