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HEAT-RESISTANT MATERIAL AND HOT STRUCTURE MEMBER BOTH FOR SPACE SHUTTLE, SPACE SHUTTLE, AND METHOD FOR PRODUCING HEAT-RESISTANT MATERIAL FOR SPACE SHUTTLE
HEAT-RESISTANT MATERIAL AND HOT STRUCTURE MEMBER BOTH FOR SPACE SHUTTLE, SPACE SHUTTLE, AND METHOD FOR PRODUCING HEAT-RESISTANT MATERIAL FOR SPACE SHUTTLE
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机译：用于航天飞机外壳的耐热材料和热结构构件，航天飞机外壳以及用于航天飞机外壳的耐热材料的制造方法
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摘要
An inexpensive high temperature oxidation resistant material for spacecraft, having a higher heat resistance than a conventional oxidation resistant material of a silicon carbide coating system, which may be readily formed into a desired shape, a hot structure part including the oxidation resistant material for spacecraft, a spacecraft provided with the hot structure part, and a method for producing the oxidation resistant material for spacecraft are provided. The oxidation resistant material for spacecraft includes a ceramic material in which silicon carbide is included in zirconium boride. The method for producing the oxidation resistant material for spacecraft includes the steps of including SiC in zirconium boride, and molding by means of a normal pressure sintering method.
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