Works matching Ion rockets
Results: 63
A novel rocket borne ion mass spectrometer with large mass range: instrument description and first flight results.
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- Atmospheric Measurement Techniques Discussions, 2020, p. 1, doi. 10.5194/amt-2020-203
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- Article
A novel rocket-borne ion mass spectrometer with large mass range: instrument description and first-flight results.
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- Atmospheric Measurement Techniques, 2021, v. 14, n. 2, p. 983, doi. 10.5194/amt-14-983-2021
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- Article
Rocket measurements of positive ions during polar mesosphere winter echo conditions.
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- Atmospheric Chemistry & Physics Discussions, 2006, v. 6, n. 4, p. 7093, doi. 10.5194/acpd-6-7093-2006
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Measurement report: Rocket-borne measurements of large ions in the mesosphere and lower thermosphere – detection of meteor smoke particles.
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- Atmospheric Chemistry & Physics, 2025, v. 25, n. 1, p. 383, doi. 10.5194/acp-25-383-2025
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- Article
Rocket measurements of positive ions during polar mesosphere winter echo conditions.
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- Atmospheric Chemistry & Physics, 2006, v. 6, n. 12/4, p. 5515, doi. 10.5194/acp-6-5515-2006
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- Article
Rocket measurements of positive ions during polar mesosphere winter echo conditions.
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- Atmospheric Chemistry & Physics, 2006, v. 6, n. 12/2, p. 5515, doi. 10.5194/acp-6-5515-2006
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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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- Article
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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- 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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- 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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- Article
To boldly and relativistically go.
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- EE: Evaluation Engineering, 2016, v. 55, n. 12, p. 28
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- Article
Comparison of Oxidation and Microstructure of Warm-Sprayed and Cold-Sprayed Titanium Coatings.
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- Journal of Thermal Spray Technology, 2012, v. 21, n. 3/4, p. 550, doi. 10.1007/s11666-011-9703-4
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- Article
Impact of plasma sheath on rocket-based E-region ion measurements.
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- Astrophysics & Space Science, 2015, v. 355, n. 1, p. 23, doi. 10.1007/s10509-014-2150-1
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- Article
W. H. T. Loh, Applied Physics and Engineering. Volume 7: Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design. XVII + 765 S. m. 203 Fig. Berlin/Heidelberg/New York 1968. Springer-Verlag. Preis geb. DM 99,20 .
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- ZAMM -- Journal of Applied Mathematics & Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1970, v. 50, n. 6, p. 439, doi. 10.1002/zamm.19700500636
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- Article
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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- Article
Nitric oxide height distribution in the lower ionosphere from rocket ion composition results over a southern temperate latitude station.
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- Journal of Geophysical Research. Space Physics, 1979, v. 84, n. A9, p. 5267, doi. 10.1029/JA084iA09p05267
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Particle ionization rates from total solar eclipse rocket ion composition results in the South Atlantic Geomagnetic Anomaly.
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- Journal of Geophysical Research. Space Physics, 1979, v. 84, n. A8, p. 4328, doi. 10.1029/JA084iA08p04328
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Rocket-borne measurements of particles and ion convection in dayside aurora.
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- Journal of Geophysical Research. Space Physics, 1978, v. 83, n. A5, p. 2195, doi. 10.1029/JA083iA05p02195
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A determination of F region convective electric fields from rocket measurements of ionospheric thermal ion spectra.
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- Journal of Geophysical Research. Space Physics, 1978, v. 83, n. A3, p. 1055, doi. 10.1029/JA083iA03p01055
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SERSIO: Svalbard EISCAT Rocket Study of Ion Outflows.
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- Journal of Geophysical Research. Space Physics, 2007, v. 112, n. A8, p. n/a, doi. 10.1029/2006JA011942
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- Article
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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The AMICIST auroral sounding rocket: A comparison of transverse ion acceleration mechanisms.
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- Geophysical Research Letters, 1996, v. 23, n. 23, p. 3293, doi. 10.1029/96GL02688
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Noctilucent clouds and regions with polar mesospheric summer echoes studied by means of rocket-borne electron and ion DC-probes.
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- Geophysical Research Letters, 1993, v. 20, n. 20, p. 2303, doi. 10.1029/93GL02048
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- Article
Bursts of transverse ion acceleration at rocket altitudes.
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- Geophysical Research Letters, 1992, v. 19, n. 4, p. 413, doi. 10.1029/92GL00091
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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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- Article
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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Measuring the seeds of ion outflow: Auroral sounding rocket observations of low-altitude ion heating and circulation.
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- Journal of Geophysical Research. Space Physics, 2016, v. 121, n. 2, p. 1587, doi. 10.1002/2015JA021536
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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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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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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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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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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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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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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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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
Numerical Modeling and GNSS Observations of Ionospheric Depletions Due To a Small‐Lift Launch Vehicle.
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- Space Weather: The International Journal of Research & Applications, 2023, v. 21, n. 9, p. 1, doi. 10.1029/2023SW003563
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Highly efficient ZnO nanoflowers for the removal of highly toxic aqueous Pb(II) and Cr(VI).
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- Journal of the Iranian Chemical Society, 2023, v. 20, n. 11, p. 2821, doi. 10.1007/s13738-023-02878-8
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Ion-Beam Sources Based on Solid Electrolytes for Aerospace Applications and Ion-Beam Technologies <italic>(Review)</italic>.
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- Instruments & Experimental Techniques, 2018, v. 61, n. 2, p. 159, doi. 10.1134/S0020441218020100
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Recent advances in the synthesis, biological activities and various applications of ferrocene derivatives.
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- Applied Organometallic Chemistry, 2017, v. 31, n. 8, p. n/a, doi. 10.1002/aoc.3664
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MICROBIOLOGICAL QUALITY OF LEAFY GREEN VEGETABLES SOLD IN THE LOCAL MARKET OF SAUDI ARABIA.
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- Italian Journal of Food Science / Rivista Italiana di Scienza degli Alimenti, 2013, v. 25, n. 4, p. 446
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Rocket (Eruca vesicaria (L.) Cav.) vs. Copper: The Dose Makes the Poison?
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- Molecules, 2022, v. 27, n. 3, p. 711, doi. 10.3390/molecules27030711
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