Deep Space Flight of Microwave Discharge Ion Engines onboard Hayabusa
スポンサーリンク
概要
著者
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Funaki I
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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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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NISHIYAMA Kazutaka
Institute of Space and Astronautical Science
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KUNINAKA Hitoshi
Institute of Space and Astronautical Science
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Nishiyama Kazutaka
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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Yamada Tetsuya
Institute Of Space And Astronautical Science
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Yamada Tetsuya
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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FUNAKI Ikko
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
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Kawaguchi Jun'ichiro
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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
- Thermal Responses of Ablator for Reentry Capsules with Superorbital Velocity
- An Experimental Study on the Boundary Layer Transition due to Gas Injection from Capsule-shape Body Surface
- Research and Development of Magnetoplasmadynamic Arcjets for Future High-Power Space Applications
- System Description and Reentry Operation Scenario of MUSES-C Reentry Capsule
- Thermal Protection System of the Reentry Capsule with Superorbital Velocity
- 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
- Nonequilibrium Temperatures Measurement in an Arc-Heated Airflow by the Optical Diagnostic Method
- Arc Heating Facility and Test Technique for Planetary Entry Missions
- DSMC-PIC Analysis of a Plume from MUSES-C Ion Engines