发明名称 スラスタ装置及び宇宙機
摘要 Of the constituting parts of a support structure (20) for a chamber (8) holding a catalyst layer which can reach high temperature, a chamber flange (24), fasteners (36a, 36b, 36c), an introduction pipe (6) conveying hydrazine and an introduction pipe flange (26) are made of a Co-Ni alloy resistant to high temperature, and a propellant valve flange (22) and columns (30a, 30b, 30c) arranged between the chamber and a propellant valve (4) which needs to be kept at low temperature as compared with the catalyst layer are made of a Ti alloy having a high thermal insulating capability.
申请公布号 JP5992722(B2) 申请公布日期 2016.09.14
申请号 JP20120113428 申请日期 2012.05.17
申请人 株式会社IHIエアロスペース 发明人 長尾 徹;森田 直樹
分类号 F02K9/68;F02K9/94 主分类号 F02K9/68
代理机构 代理人
主权项
地址