DEVELOPMENT OF MICROWAVE DISCHARGE ION ENGINE SYSTEM FOR ASTEROID SAMPLE AND RETURN MISSION MUSES-C
スポンサーリンク
概要
著者
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Satori Shin
Hokkaido Institute Of Technology Sapporo
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Funaki I
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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Funaki Ikkoh
Institute Of Space And Astronautical Science Jaxa
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Shimizu Yukio
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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SHIMIZU Yukio
The Institute of Space and Astronautical Science
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TOKI Kyoichiro
Institute of Space and Astronautical Science
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SATORI Shin
Institute of Space and Astronautical Science
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KUNINAKA Hitoshi
Institute of Space and Astronautical Science
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Toki Kyoichiro
Tokyo University Of Agriculture And Technology
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Toki K
The Institute Of Space And Astronautical Science
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Funaki Ikkoh
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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Kuninaka Hitoshi
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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Shimizu Yukio
Institute Of Space And Astronautical Science
関連論文
- Experimental Investigation of Carbon Contamination Inside Discharge Chamber of Ion Thruster
- GROUND TESTS AND SPACE TESTS OF A MAGNETOPLASMADYNAMIC ARCJET THRUSTER SYSTEM
- Electron Cyclotron Resonance Ion Source for Ion Thruster
- Two Dimensional Analysis of High Volatage Solar Array Interfering with Ionospheric Plasma
- Design and Initial Operation of an Experimental Simulator of Magnetic Sail
- Development of Microwave Ion Engine System for MUSES-C Mission
- DEVELOPMENT OF MICROWAVE DISCHARGE ION ENGINE SYSTEM FOR ASTEROID SAMPLE AND RETURN MISSION MUSES-C
- Research and Development of Magnetoplasmadynamic Arcjets for Future High-Power Space Applications
- DSMC-PIC Analysis of a Plume from MUSES-C Ion Engines
- Deep Space Flight of Microwave Discharge Ion Engines onboard Hayabusa
- Low-Power Microwave Electron Source for Ion Engine Neutralizer
- SAIL PROPULTION USING THE SOLAR WIND
- DSMC-PIC Analysis of a Plume from MUSES-C Ion Engines
- Preliminary Investigation of Electromagnetic Thrust Characteristics in Electrodeless Compact Helicon Plasma Thruster