79 research outputs found

    A dehydrated space-weathered skin cloaking the hydrated interior of Ryugu

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    Without a protective atmosphere, space-exposed surfaces of airless Solar System bodies gradually experience an alteration in composition, structure and optical properties through a collective process called space weathering. The return of samples from near-Earth asteroid (162173) Ryugu by Hayabusa2 provides the first opportunity for laboratory study of space-weathering signatures on the most abundant type of inner solar system body: a C-type asteroid, composed of materials largely unchanged since the formation of the Solar System. Weathered Ryugu grains show areas of surface amorphization and partial melting of phyllosilicates, in which reduction from Fe3+ to Fe2+ and dehydration developed. Space weathering probably contributed to dehydration by dehydroxylation of Ryugu surface phyllosilicates that had already lost interlayer water molecules and to weakening of the 2.7 µm hydroxyl (–OH) band in reflectance spectra. For C-type asteroids in general, this indicates that a weak 2.7 µm band can signify space-weathering-induced surface dehydration, rather than bulk volatile loss

    Experimental Study for Enhancement Thrust Force of the ECR Ion Thruster μ10

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    Plasma Diagnostics of the µ10 ECR Ion Thruster Using Optical Fiber Probes

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    In order to reveal the physical processes taking place within the ECR ion thruster " µ10 ", internal plasma diagnosis is indispensable. However, the ability of metallic probes to access microwave plasmas biased at a high voltage is limited from the standpoints of he disturbance created in the electric field and electrical isolation. This study demonstrates two kinds of plasma parameter measurements using optical fibers. Firstly, an optical fiber probe is a single-mode optical fiber. It is used to guide laser into the discharge chamber in the measurement of Xe I by the laser absorption spectroscopy. The other is an EO probe to measure the electric field of microwaves. From the both results, it can be deduced that there is plasma in the waveguide in the propellant injection from a waveguide. To improve the thrust force, it is important to suppress the electron in the waveguide

    マイクロ波放電型イオンスラスタのプラズマモード遷移に関する研究

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