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Relevant bibliographies by topics / Ion engines

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Academic literature on the topic 'Ion engines'

Author: Grafiati

Published: 4 June 2021

Last updated: 12 February 2022

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Journal articles on the topic "Ion engines"

1

Freiherr, Greg. "The Little Rocket Engine That Could." Mechanical Engineering 138, no. 08 (2016): 32–37. http://dx.doi.org/10.1115/1.2016-aug-1.

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This paper highlights advancements of a research team in the field of miniature spacecrafts and development and advantages of CubeStats. CubeSats are space age hitchhikers, that is, miniature spacecraft that fly into orbit aboard rockets whose primary payloads are full-size satellites. Paulo Lozano and his team at MIT’s Space Propulsion Lab have developed a unique kind of rocket engine for these microsatellites. The trick to building a successful ion electrospray propulsion system is to increase thrust density by jamming together as many emitters as possible. Electrospray engines also differ g

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Sorokin, A., X. Vancassel, and P. Mirabel. "Emission of ions and charged soot particles by aircraft engines." Atmospheric Chemistry and Physics Discussions 2, no. 6 (2002): 2045–74. http://dx.doi.org/10.5194/acpd-2-2045-2002.

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Abstract. In this article, a model which examines the formation and evolution of chemiions in an aircraft engine is proposed. This model which includes chemiionisation, electron thermo-emission, electron attachment to soot particles and to neutral molecules, electron-ion and ion-ion recombination, ion-soot interaction, allows the determination of the ion concentration at the exit of the combustor and at the nozzle exit of the engine. It also allows the determination of the charge of the soot particles. A comparison of the model results with the available ground-based experimental data obtained

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Sorokin, A., X. Vancassel, and P. Mirabel. "Emission of ions and charged soot particles by aircraft engines." Atmospheric Chemistry and Physics 3, no. 2 (2003): 325–34. http://dx.doi.org/10.5194/acp-3-325-2003.

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Abstract. In this article, a model which examines the formation and evolution of chemiions in an aircraft engine is proposed. This model which includes chemiionisation, electron thermo-emission, electron attachment to soot particles and to neutral molecules, electron-ion and ion-ion recombination, ion-soot interaction, allows the determination of the ion concentration at the exit of the combustor and at the nozzle exit of the engine. It also allows the determination of the charge of the soot particles. For the engine considered, the upper limit for the ion emission index EIi is of the order of

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Petrov, Nikolay, and Tamara Antonova. "Increasing the specific impulse of the ion engine by zone engineering of the solid-state field cathode." Proceedings of the Russian higher school Academy of sciences, no. 4 (January 20, 2021): 41–50. http://dx.doi.org/10.17212/1727-2769-2020-4-41-50.

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With the rapid development of space technology, the scale of human space exploration is expanding significantly. However, the growing demand for deep space travel cannot be met with conventional chemical engines. Thus, the need for new mechanisms for providing jet thrust, including electric motors, becomes clear. Electric propulsion technology has significant advantages over traditional chemical engines in deep space flight due to its characteristics such as high specific impulse, small size, long service life. A negative feature of electric motors can be called low thrust, however, firstly, i

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Mehresh, P., D. Flowers, and R. W. Dibble. "Experimental and numerical investigation of effect of fuel on ion sensor signal to determine combustion timing in homogeneous charge compression ignition engines." International Journal of Engine Research 6, no. 5 (2005): 465–74. http://dx.doi.org/10.1243/146808705x30404.

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Homogeneous charge compression ignition (HCCI) engines offer promise owing to low emissions and high efficiency. However, the control of the combustion process in HCCI engines, specifically the control of the start of combustion (SOC) or ignition timing, remains a challenge. Piezoelectric pressure transducers are used in research engines for determination of the start of combustion; however, these pressure transducers are too expensive and fragile for applications in commercial engines. Recent work by the authors as well as other investigators has shown the potential of inexpensive ion sensors

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Budko, Artem Yur’evich, M. Yu Medvedev, and Vladimir Vladimirovich Matsiborko. "Improving the Efficiency of Power Generation Plants Based on Internal Combustion Engines." Applied Mechanics and Materials 752-753 (April 2015): 941–45. http://dx.doi.org/10.4028/www.scientific.net/amm.752-753.941.

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This paper describes a method developed by the authors for the detection and estimation of knock intensity in the cylinders of internal combustion engines. The method is based on the spectral analysis of the ion current signal, which is detected within the combustion chamber of the engine. The method allows estimation of the total wave packet energy for different waves speed and frequency. The estimation results of wave’s energy arising in the normal and knock combustion to engine VAZ 2110 are also presented in the paper work.

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Miao, Jian-Guo, Chun-Wang Wu, Wei Wu, and Ping-Xing Chen. "Entropy Exchange and Thermodynamic Properties of the Single Ion Cooling Process." Entropy 21, no. 7 (2019): 650. http://dx.doi.org/10.3390/e21070650.

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A complete quantum cooling cycle may be a useful platform for studying quantum thermodynamics just as the quantum heat engine does. Entropy change is an important feature which can help us to investigate the thermodynamic properties of the single ion cooling process. Here, we analyze the entropy change of the ion and laser field in the single ion cooling cycle by generalizing the idea in Reference (Phys. Rev. Lett. 2015, 114, 043002) to a single ion system. Thermodynamic properties of the single ion cooling process are discussed and it is shown that the Second and Third Laws of Thermodynamics

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Fujita, Kazuhisa. "Air Intake Performance of Air Breathing Ion Engines." JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 52, no. 610 (2004): 514–21. http://dx.doi.org/10.2322/jjsass.52.514.

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WATANABE, Hiroki, Tomoyuki HATAKEYAMA, Masatoshi IRIE, et al. "Study on Radio Frequency Cathode for Ion Engines." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN 7, ists26 (2009): Pb_53—Pb_58. http://dx.doi.org/10.2322/tstj.7.pb_53.

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KUNINAKA, Hitoshi. "Microwave Discharge Ion Engines Onboard Hayabusa Asteroid Explorer." Hyomen Kagaku 33, no. 12 (2012): 669–74. http://dx.doi.org/10.1380/jsssj.33.669.

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Dissertations / Theses on the topic "Ion engines"

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Starling, Dan A. "Propellant feed control for ion engines." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1996. http://handle.dtic.mil/100.2/ADA316748.

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Starling, Dan A. Jr. "Propellant feed control for ion engines." Thesis, Monterey, California. Naval Postgraduate School, 1996. http://hdl.handle.net/10945/8868.

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Approved for public release, distribution is unlimited<br>An overview of space electric propulsion (SEP) is presented. Methods of throttling the power levels of electrostatic and electromagnetic thrusters are discussed. Particular attention is given to the concept of thermally- throttling propellant flow using the temperature-viscosity characteristics of xenon gas. The thermoproperties of xenon gas as a function of temperature are determined, and the flow regimes of the propellant at the mass flow rates of interest are studied. The propellant flow is presented separately as Fanno flow and as R

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Gruber, J. R. "A study of erosion due to low-energy sputtering in the discharge chamber of the Kaufman ion thruster." Thesis, University of Oxford, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.249396.

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Panousakis, Dimosthenis. "Ion current sensing for controlled auto ignition in internal combustion engines." Thesis, Loughborough University, 2009. https://dspace.lboro.ac.uk/2134/8145.

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Envirom-nental pollution is a subject that needs urgent addressing. Since the internal combustion engine has its fair share of accountability on this, research on techniques for increasing engine efficiency and emissions is necessary. Controlled Auto Ignition is a promising combustion mode, which increases fuel efficiency while also reducing NOx emissions to negligible levels. This Thesis concentrates on the implementation of this mode through experimental research, on an engine equipped with a fully variable valvetrain. Investigation of the operational window, emissions, fuel consumption, the

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Holub, Anna, and Jie Liu. "Recognizing Combustion Variability for Control of Gasoline Engine Exhaust Gas Recirculation using Information from the Ion Current." Thesis, Halmstad University, School of Information Science, Computer and Electrical Engineering (IDE), 2006. http://urn.kb.se/resolve?urn=urn:nbn:se:hh:diva-235.

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<p>The ion current measured from the spark plug in a spark ignited combustion engine is used </p><p>as basis for analysis and control of the combustion variability caused by exhaust gas </p><p>recirculation. Methods for extraction of in-cylinder pressure information from the ion </p><p>current are analyzed in terms of reliability and processing efficiency. A model for the </p><p>recognition of combustion variability using this information is selected and tested on both </p><p>simulated and car data.</p>

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Ogunjobi, Taiwo A. "Computational Study of Ring-Cusp Magnet Configurations that Provide Maximum Electron Confinement." Wright State University / OhioLINK, 2006. http://rave.ohiolink.edu/etdc/view?acc_num=wright1166226698.

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Botha, Johannes Rudolf. "Design of an RF ion thruster." Thesis, Stellenbosch : Stellenbosch University, 2014. http://hdl.handle.net/10019.1/86267.

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Thesis (MEng)--Stellenbosch University, 2014.<br>ENGLISH ABSTRACT: Recent years have seen a decline in the rate of space exploration due to the inefficiency of chemical rockets. Therefore alternative fuel efficient propulsion methods are being sought to enable cost effective deep space exploration. The high fuel efficiency of electric thrusters enable a spacecraft to travel further, faster and cheaper than any other propulsion technology available. Thus electric propulsion has become the propulsion of choice for scientists and engineers. A typically electric thruster contains some sort of

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Rodrigues, Junior Robério. "Avaliação comparativa de recobrimentos superficiais para tuchos de válvula através de ensaios de desgaste." [s.n.], 2010. http://repositorio.unicamp.br/jspui/handle/REPOSIP/263572.

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Orientador: Cecília Amélia de Carvalho Zavaglia<br>Dissertação (mestrado profissional) - Universidade Estadual de Campinas, Faculdade de Engenharia Mecânica<br>Made available in DSpace on 2018-08-16T19:02:52Z (GMT). No. of bitstreams: 1 RodriguesJunior_Roberio_M.pdf: 3328140 bytes, checksum: d0f2014c71eeb448ae530ee5df6b8479 (MD5) Previous issue date: 2010<br>Resumo: Com o intuito de avaliar a eficiência de diferentes recobrimentos superficiais aplicados a tuchos de válvulas - um componente utilizado em motores à combustão - foram propostos alguns recobrimentos que foram comparados a um recob

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Benyo, Theresa L. "Analytical and Computational Investigations of a Magnetohydrodynamic (MHD) Energy-Bypass System for Supersonic Turbojet Engines to Enable Hypersonic Flight." Kent State University / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=kent1369153719.

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Gustafsson, Karin. "Ion Current Dependence on Operating Condition and Ethanol Ratio." Thesis, Linköping University, Department of Electrical Engineering, 2006. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-8053.

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<p>This masters thesis investigates the possibility to estimate the ethanol content in the fuel using ion currents. Flexible fuel cars can be run on gasoline-ethanol blends with an ethanol content from0 to 85 percentage. It is important for the engine control system to have information about the fuel. In todays cars the measurements of the fuel blend are done by a sensor. If it is possible to do this with ion currents this can be used to detect if the sensor is broken, and then estimate the ethanol content until the sensor gets fixed. The benefit</p><p>of using ion currents is that the signal

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Books on the topic "Ion engines"

1

Starling, Dan A. Propellant feed control for ion engines. Naval Postgraduate School, 1996.

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2

Foster, John E. Inter-cusp ion and electron transport in a NSTAR-derivative ion thruster. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Foster, John E. Inter-cusp ion and electron transport in a NSTAR-derivative ion thruster. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Foster, John E. Inter-cusp ion and electron transport in a NSTAR-derivative ion thruster. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Foster, John E. Inter-cusp ion and electron transport in a NSTAR-derivative ion thruster. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Foster, John E. Internal plasma properties and enhanced performance of an 8-cm ion thruster discharge. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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Rawlin, Vincent K. Thermal environmental testing of NSTAR engineering model ion thrusters. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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International Electric Propulsion Conference (24th 1995 Moscow, Russia). Proceedings of the 24th International Electric Propulsion Conference: IEPC. s.n., 1995.

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Stuart, Thomas A. Study of a high voltage ion engine power supply: NASA grant NAG3-1576. National Aeronautics and Space Administration, 1996.

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Foster, John E. Enhanced discharge performance in a ring cusp plasma source. National Aeronautics and Space Administration, Glenn Research Center, 2000.

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Book chapters on the topic "Ion engines"

1

Weißgerber, Tycho, and Gregor Kortendiek. "Spark Control for Ion Current Sensing." In Ignition Systems for Gasoline Engines. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-45504-4_12.

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Sheppard, C. G. W., and E.-S. A. A. Ibrahim. "S. I. Engine Ion Probe Diagnostics." In Instrumentation for Combustion and Flow in Engines. Springer Netherlands, 1989. http://dx.doi.org/10.1007/978-94-009-2241-9_19.

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Li, Ruiguang, Meng Shen, Hao Yu, Chao Li, Pengyu Duan, and Lihuang Zhu. "A Survey on Cyberspace Search Engines." In Communications in Computer and Information Science. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-33-4922-3_15.

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AbstractThis paper introduces the concept of cyberspace search engine, and makes a deep survey on 5 well-known search engines, say Shodan, Censys, BinaryEdge, ZoomEye and Fofa, by querying official websites, analyzing APIs, and making academic research. We discuss the following items in details: Supporting internet protocols, Total amounts of detected devices, Device information, Scanning frequency, System architecture, The third party databases, Probes distribution, etc. We give a comprehensive comparison of the detecting abilities and working principles of the cyberspace search engines.

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Calabretta, Michele, Alessandro Sitta, Salvatore Massimo Oliveri, and Gaetano Sequenzia. "Simulation of Dynamic Stresses on High Performance Engine Valve Spring System Considering Coil Clashing Effect." In Lecture Notes in Mechanical Engineering. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-70566-4_18.

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AbstractThe valve train plays a major role in the performance of internal combustion engines by controlling the combustion process and it is therefore one of the key aspects for increasing the efficiency of combustion engines. Considering the dynamics, the spring force must be high enough to reliably close the valve preventing from seating bouncing due to surge modes after the valve closure. On the other side, the spring force should be kept as low as possible in order to reduce the engine friction losses and consequently the fuel consumption. In the high-performance engines, the valve springs have to be designed and optimized for sustaining higher stresses with compact dimensions leading to critical material and manufacturing processes. This requires a reduction of moving masses and a strong focus on design and process optimization of the coil springs for reducing the mechanical load and the friction losses at low engine speed. At the same time, valve train should be reliable at high engine speed. The calculation of stresses and contact forces for moving parts under dynamic load is essential for durability analysis. A method to calculate the contact of moving masses is described and proposed to justify valve motions experimental results. To fully understand the failure mechanism of test bed reliability trials, the dynamic stresses have been calculated modeling the real springs’ shape. The contact forces have been reproduced considering the coil clash effects and the dynamic behavior of the flexible spring.

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Fiedler, Torben, Joachim Rösler, Martin Bäker, et al. "Mechanical Integrity of Thermal Barrier Coatings: Coating Development and Micromechanics." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_19.

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Abstract To protect the copper liners of liquid-fuel rocket combustion chambers, a thermal barrier coating can be applied. Previously, a new metallic coating system was developed, consisting of a NiCuCrAl bond-coat and a Rene 80 top-coat, applied with high velocity oxyfuel spray (HVOF). The coatings are tested in laser cycling experiments to develop a detailed failure model, and critical loads for coating failure were defined. In this work, a coating system is designed for a generic engine to demonstrate the benefits of TBCs in rocket engines, and the mechanical loads and possible coating failure are analysed. Finally, the coatings are tested in a hypersonic wind tunnel with surface temperatures of 1350 K and above, where no coating failure was observed. Furthermore, cyclic experiments with a subscale combustion chamber were carried out. With a diffusion heat treatment, no large-scale coating delamination was observed, but the coating cracked vertically due to large cooling-induced stresses. These cracks are inevitable in rocket engines due to the very large thermal-strain differences between hot coating and cooled substrate. It is supposed that the cracks can be tolerated in rocket-engine application.

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Itterheim, Steffen, and Andreas Löw. "Physics Engines." In Learn cocos2D Game Development with iOS 5. Apress, 2011. http://dx.doi.org/10.1007/978-1-4302-3814-0_12.

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Badescu, Viorel. "Diesel Engines." In Optimal Control in Thermal Engineering. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-52968-4_20.

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Badescu, Viorel. "Photochemical Engines." In Optimal Control in Thermal Engineering. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-52968-4_22.

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Palocz-Andresen, Michael. "Airplane Engines." In Decreasing Fuel Consumption and Exhaust Gas Emissions in Transportation. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-11976-7_10.

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Palocz-Andresen, Michael. "Vehicle Engines." In Decreasing Fuel Consumption and Exhaust Gas Emissions in Transportation. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-11976-7_9.

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Conference papers on the topic "Ion engines"

1

Janson, S. "Microwave interferometry for ion engines." In 30th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-2741.

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Kubach, Heiko, Amin Velji, Ulrich Spicher, and Wolfgang Fischer. "Ion Current Measurement in Diesel Engines." In 2004 Powertrain & Fluid Systems Conference & Exhibition. SAE International, 2004. http://dx.doi.org/10.4271/2004-01-2922.

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BROPHY, JOHN. "Near-term, 100-kW class ion engines." In Conference on Advanced SEI Technologies. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3566.

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Yamamoto, Naoji, Taichi Morita, Ikkoh Funaki, Masakatsu Nakano, and Yasushi Ohkawa. "Demonstration of Wide Throttling Range Ion Engines." In 2018 Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-4815.

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Fearn, David. "The Future Development of Gridded Ion Engines." In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-4714.

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ZARNITZ, F., K. GROH, H. LOEB, J. FELL, and F. WEBER. "Development status of the RIT ion engines." In 21st International Electric Propulsion Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2671.

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Förster, Jürgen, Achim Günther, Markus Ketterer, and Klaus-Jürgen Wald. "Ion Current Sensing for Spark Ignition Engines." In International Congress & Exposition. SAE International, 1999. http://dx.doi.org/10.4271/1999-01-0204.

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Mehresh, P., R. W. Dibble, and D. Flowers. "EGR effect on Ion Signal in HCCI Engines." In 2005 SAE Brasil Fuels & Lubricants Meeting. SAE International, 2005. http://dx.doi.org/10.4271/2005-01-2126.

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Kuninaka, Hitoshi, and Andrew V. Pakhomov. "Microwave Discharge Ion Engines onboard Hayabusa Asteroid Explorer." In BEAMED ENERGY PROPULSION: Fifth International Symposium on Beamed Energy Propulsion. AIP, 2008. http://dx.doi.org/10.1063/1.2931929.

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Przybylowski, J. N., J. E. Polk, and J. E. Shepherd. "Evidence for ion acceleration by oscillations in the discharge plasma of ion engines." In 2009 IEEE 36th International Conference on Plasma Science (ICOPS). IEEE, 2009. http://dx.doi.org/10.1109/plasma.2009.5227732.

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Reports on the topic "Ion engines"

1

Cheng, Wai, Victor Wong, Michael Plumley, et al. Lubricant Formulations to Enhance Engine Efficiency in Modern Internal Combustion Engines. Office of Scientific and Technical Information (OSTI), 2017. http://dx.doi.org/10.2172/1351980.

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Frame, Edwin A., Adam C. Brandt, Ruben Sr A. Alvarez, Allen S. Comfort, and Luis A. Villahermosa. Feasibility of Using Full Synthetic Low Viscosity Engine Oil at High Ambient Temperatures in U.S. Army Engines. Defense Technical Information Center, 2011. http://dx.doi.org/10.21236/ad1007443.

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Sugita, Takayuki. Compressed Air as a Quality and Pollution Free Fuel Substitute in Reciprocating Engines - Effective Solutions to Improve Engine Performance. SAE International, 2011. http://dx.doi.org/10.4271/2011-32-0509.

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Tubman, Michael, and Timothy Welp. Evaluation Tests of Select Fuel Additives for Potential Use in U.S. Army Corps of Engineers Diesel Engines. Defense Technical Information Center, 2016. http://dx.doi.org/10.21236/ad1013242.

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Eidler, Phillip. Dueco Plug-In Hybrid Engines. Office of Scientific and Technical Information (OSTI), 2011. http://dx.doi.org/10.2172/1055765.

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Xu, Hongming, Trevor Wilson, Stan Wallace, et al. Progress in FORESIGHT Homogeneous Autoignition Engines. SAE International, 2005. http://dx.doi.org/10.4271/2005-08-0221.

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Allen, Jr, and John J. Air Force Civil Engineers in Joint Engineer Operations: Validating the Concept and Incorporating Lessons Learned. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada513943.

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Dodge, L., and D. Naegeli. Combustion Characterization of Methylal in Reciprocating Engines. Office of Scientific and Technical Information (OSTI), 1994. http://dx.doi.org/10.2172/10157045.

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Dodge, L., and D. Naegeli. Hydrogen-air mixing evaluation in reciprocating engines. Office of Scientific and Technical Information (OSTI), 1994. http://dx.doi.org/10.2172/10156770.

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Failla, Charles C., and Andrew A. Pouring. Kerosene Base Fuels in Small Gasoline Engines. Defense Technical Information Center, 1991. http://dx.doi.org/10.21236/ada244846.

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