Works matching DE "ION rockets"
Results: 26
Chaos control with ion propulsion.
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- Astronomische Nachrichten, 2017, v. 338, n. 5, p. 536, doi. 10.1002/asna.201713222
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Effect of Orifice Diameter on the Performance of a Miniature Microwave Neutralizer.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2017, v. 60, n. 4, p. 259, doi. 10.2322/tjsass.60.259
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Modeling Plasma via Electron Impact Ionization.
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- Aerospace (MDPI Publishing), 2018, v. 5, n. 1, p. 2, doi. 10.3390/aerospace5010002
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To boldly and relativistically go.
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- EE: Evaluation Engineering, 2016, v. 55, n. 12, p. 28
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Studies of Dust and Discharges around a Martian Rover with Onboard Hazard Analyses using Electromagnetic and Acoustic Wave Measurements.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 41
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Optimization of Plasma Production with Impedance Analysis for a Micro RF Ion Thruster.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 63
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Self-Consistent Numerical 0D/3D Hybrid Modeling of Radio-Frequency Ion Thrusters.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 23
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Initial Flight Operations of the Miniature Propulsion System Installed on Small Space Probe: PROCYON.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 13
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Development of a Radio-Frequency Generator for RF Ion Thrusters.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 33
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Feasibility Study on Numerical Life Qualification of Ion Thruster's Ion Optics Using the JIEDI Tool.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 65
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Investigation of Plasma Characteristics and Ion Beam Extraction for a Micro RF Ion Thruster.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 13
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Neutral Density Measurement of Ion Thruster with Differential Pressure Gauge.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 73
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- Article
Exotic Propellant for Continuous Wave Laser Propulsion.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 47
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- Article
Engineering Model of the Miniature Ion Propulsion System for the Nano-satellite: HODOYOSHI-4.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 19
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- Article
Measurement of Microwave Absorbance by Plasma of a Miniature Microwave Discharge Ion Thruster.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 91
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Characterization and Improvement of a Laser-Assisted Pulsed Plasma Thruster.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 25
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- Article
Development of a Low Power Multipole Confined Microwave Plasma Ion Thruster.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 7
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- Article
Editorial for Volume 7 Number 1: The Space Transportation.
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- International Journal of Combinatorial Optimization Problems & Informatics, 2016, v. 7, n. 1, p. 1
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Design of high efficiency and high thrust grid system for ion thruster.
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- Journal of Electromagnetic Waves & Applications, 2017, v. 31, n. 17, p. 1816, doi. 10.1080/09205071.2017.1349002
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Dawn launch dawning.
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- Astronomy & Geophysics, 2007, v. 48, n. 3, p. 3.06, doi. 10.1111/j.1468-4004.2007.48304_12.x
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- Article
Lifter - High voltage plasma levitation device.
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- Caderno Brasileiro de Ensino de Física, 2015, v. 37, n. 3, p. 3307-1, doi. 10.1590/S1806-11173731869
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Modelling ion propulsion plume interactions with spacecraft in formation flight.
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- Aeronautical Journal, 2010, v. 114, n. 1157, p. 417, doi. 10.1017/S0001924000003894
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The Effect of the Discharge Chamber Structure on the Performance of a 5 cm-Diameter ECR Ion Thruster.
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- Progress in Electromagnetics Research Letters, 2018, v. 75, p. 91, doi. 10.2528/pierl18030703
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- Article
On the mechanical behavior of carbon-carbon optic grids determined using a bi-axial optical extensometer.
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- Journal of Materials Science, 2004, v. 39, n. 14, p. 4495, doi. 10.1023/B:JMSC.0000034143.30654.b8
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Performance of an iodine-fueled radio-frequency ion-thruster.
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- European Physical Journal D (EPJ D), 2018, v. 72, n. 1, p. 1, doi. 10.1140/epjd/e2017-80498-5
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Development of ion thruster IT-500.
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- European Physical Journal D (EPJ D), 2017, v. 71, n. 5, p. 1, doi. 10.1140/epjd/e2017-70644-6
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- Article