- 专利标题： HAN-BASED PROPELLANT DECOMPOSITION CATALYST, PRODUCTION METHOD THEREFOR, AND MONOPROPELLANT THRUSTER USING SAME
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申请号： EP17834495.8申请日： 2017-07-27
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公开(公告)号： EP3492168A1公开(公告)日： 2019-06-05
- 发明人: KAMATA Hiroyuki , IGARASHI Shinji , YAMAMOTO Kengo , FUKUCHI Aporo
- 申请人： IHI Corporation , IHI Aerospace Co., Ltd.
- 申请人地址： 1-1 Toyosu 3-chome Koto-ku Tokyo 135-8710 JP
- 专利权人： IHI Corporation,IHI Aerospace Co., Ltd.
- 当前专利权人： IHI Corporation,IHI Aerospace Co., Ltd.
- 当前专利权人地址： 1-1 Toyosu 3-chome Koto-ku Tokyo 135-8710 JP
- 代理机构： Grünecker Patent- und Rechtsanwälte PartG mbB
- 优先权： JP2016150512 20160729
- 国际公布： WO2018021493 20180201
- 主分类号： B01J23/656
- IPC分类号： B01J23/656 ; B01J32/00 ; B01J35/10 ; B01J37/02 ; B01J37/08 ; B01J37/18 ; B64G1/26
摘要：
There are provided a stable HAN-based propellant decomposition catalyst in which the heat resistance is sufficient and the change in HAN-based propellant decomposition activity over time is also small so that a HAN-based propellant having low toxicity can be used for a thruster, and a method for producing the same, and a one-component thruster including a HAN-based propellant decomposition catalyst. A HAN-based propellant decomposition catalyst containing a hexaaluminate type oxide containing a platinum group element, and a method for producing the same, and a one-component thruster including a HAN-based propellant decomposition catalyst are used.
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