Budget Amount *help |
¥4,810,000 (Direct Cost: ¥3,700,000、Indirect Cost: ¥1,110,000)
Fiscal Year 2018: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
Fiscal Year 2017: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
Fiscal Year 2016: ¥1,950,000 (Direct Cost: ¥1,500,000、Indirect Cost: ¥450,000)
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Outline of Final Research Achievements |
In order to investigate of the oxidation behaviors of Thermal Protection System (TPS) for space planes, the development of the arc-heated wind tunnel was conducted. ZrN, TiN, TiCN coatings were applied on the Zr cathode using ion plating method and Cu-Cr alloy was coated on the Cu anode expecting for reducing of the electrodes erosion. Pre-heating of the cathode with laser was also effective for preventing the erosion. Dynamic oxidation of the TPS were conducted using laser driven plasma wind tunnel.
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