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	High-density ceramic matrix composite material used as hypersonic aircraft surface insulation layer, is obtained by hot-press sintering zirconium diboride-zirconium disilicide-tungsten carbide mixed powder having specified purity.
	LI J DAI J SHA J WEI Z ZHANG Z
	2014
公开日期	2014-02-05
URL标识	查看原文
申请日期	2013-09-27
内容类型	专利
URI标识	http://www.corc.org.cn/handle/1471x/4516720
专题	大连理工大学
作者单位	UNIV DALIAN TECHNOLOGY (UYDA-C
推荐引用方式 GB/T 7714	LI J DAI J SHA J WEI Z ZHANG Z. High-density ceramic matrix composite material used as hypersonic aircraft surface insulation layer, is obtained by hot-press sintering zirconium diboride-zirconium disilicide-tungsten carbide mixed powder having specified purity.. 2014-01-01.

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