发明名称 COMPOSITION FOR HEAT INSULATOR, HEAT INSULATOR, AND SPACECRAFT EQUIPPED THEREWITH
摘要 A composition for a heat insulator, a heat insulator, and a spacecraft equipped with the heat insulator are provided which are able to satisfy a desired level of heat insulation performance while suppressing recession. The composition for a heat insulator comprises a fibrous substance, inorganic foam particles, a thermosetting resin and a foaming agent, wherein the fibrous substance includes at least a first fibrous substance, and a second fibrous substance composed of a material different from the first fibrous substance, the melting point of the first fibrous substance is higher than the melting point of the second fibrous substance, and the thermal conductivity of the second fibrous substance is lower than the thermal conductivity of the first fibrous substance.
申请公布号 US2014356571(A1) 申请公布日期 2014.12.04
申请号 US201314369846 申请日期 2013.01.16
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. ;LIGNYTE CO., LTD 发明人 Watanabe Junko;Tsukahara Aiichiro;Yamashita Masayuki;Takeda Fumihito;Higuchi Hisato;Takeda Shinsuke;Hara Nagaharu
分类号 B64G1/58;C08L61/06;C08J9/00;B32B5/26;B32B5/24 主分类号 B64G1/58
代理机构 代理人
主权项 1. A composition for a heat insulator comprising a fibrous substance, inorganic foam particles, a thermosetting resin and a foaming agent, wherein the fibrous substance comprises at least a first fibrous substance, and a second fibrous substance composed of a material different from the first fibrous substance, a melting point of the first fibrous substance is higher than a melting point of the second fibrous substance, and a thermal conductivity of the second fibrous substance is lower than a thermal conductivity of the first fibrous substance.
地址 Tokyo JP